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1
THE RAYLEIGH PROBLEM IN A RADIATING ...
1966-07-01

... Title : THE RAYLEIGH PROBLEM IN A RADIATING COMPRESSIBLE GAS. PART II. PLATE MACH NUMBER LARGE. Corporate ...

DTIC Science & Technology

2
AERODYNAMICS OF SLENDER BODIES AT MACH ...
1954-05-06

... Lawrence I.: Aerodynamics of Slender Bodies at Mach Number of 3.12 and Reynolds Numbers from 2X106 to 15X106. II - Aerodynamic Load ...

DTIC Science & Technology

3
ON I, DYNAMICAL SIMILARITY AND II, INTRINSIC ...
1961-09-01

... Abstract : A discussion is presented on the constancy and similarities of dynamics such as: magnetic Reynolds number, magnetic Mach number ...

DTIC Science & Technology

4
Aerodynamic and Inlet Characteristics of the HAST I and II ...
1974-03-01

... Accession Number : AD0918103. Title : Aerodynamic and Inlet Characteristics of the HAST I and II Missiles at Mach Numbers 0.5 to 1.6. ...

DTIC Science & Technology

5
Development of Algorithms for Nonlinear Physics on Type-II ...
2007-07-01

... limitations here. Another unexpected result unearthed by the CAP runs was the dependence of the ELB on the Mach number. A ...

DTIC Science & Technology

6
EFFECT OF MACH NUMBER, REYNOLDS NUMBER, AND ...
1965-06-01

... Title : EFFECT OF MACH NUMBER, REYNOLDS NUMBER, AND THICKNESS RATIO ON ... The tests were conducted at Mach numbers ranging from ...

DTIC Science & Technology

7
Mach Number Corrections Due to Wall Effects (Mach Number ...
1974-09-10

... Title : Mach Number Corrections Due to Wall Effects (Mach Number, Obstruction) Limitations in Solid Test Sections Additional Limitations in ...

DTIC Science & Technology

8
WIND TUNNEL TESTS OF AN UNMANNED FOLDING DELTA ...
1961-12-01

... HYPERSONIC GLIDER. PART II. LATERAL STATIC STABILITY AND CONTROL AT MACH NUMBERS OF 0.80, 1.86, AND 2.87. ...

DTIC Science & Technology

9
Static Stability and Control Effectiveness of the MK-84 Modular ...
1974-07-01

... Title : Static Stability and Control Effectiveness of the MK-84 Modular Guided Glide Bomb II at Transonic Mach Numbers. ...

DTIC Science & Technology

10
Oblique Shock Wave/Turbulent Boundary Layer Interactions in ...
1978-03-01

... Accession Number : ADA057010. Title : Oblique Shock Wave/Turbulent Boundary Layer Interactions in Three Dimensions at Mach 3. Part II. ...

DTIC Science & Technology

11
Tory II-C performance as a function of flight mach number and inlet pressure recovery
1963-01-01

In a parameter study involving thrust vs. flight Mach number, M.D. Mintz has found that net jet thrust becomes a maximum at about Mach 3.66 if the Tory II-C design value of inlet pressure recovery is used at all Mach numbers. This is not a realistic situation, however, ...

DOE Information Bridge

12
Low Mach Number Modeling of Type Ia Supernovae. II. EnergyEvolution
2006-03-28

The convective period leading up to a Type Ia supernova (SNIa) explosion is characterized by very low Mach number flows, requiringhydrodynamical methods well-suited to long-time integration. We continuethe development of the low Mach number equation set for stellar scaleflows by incorporating the effects of heat ...

Energy Citations Database

13
THE MACH NUMBER AND TEMPERATURE CALIBRATION ...
1957-06-01

... Title : THE MACH NUMBER AND TEMPERATURE CALIBRATION OF AN AXISYMMETRIC, INTERMITTENT-FLOW SUPERSONIC WIND TUNNEL,. ...

DTIC Science & Technology

14
National transonic facility Mach number system
1985-01-01

The Mach number system for the Langley Research Center's National Transonic Facility was designed to

NASA Technical Reports Server (NTRS)

15
Effects of Mach Number and Reynolds Number on the ...
1947-05-01

... at relatively low free-stream Mach numbers and, before critical Mach number was reached, were almost entirely dependent on Reynolds Number. ...

DTIC Science & Technology

16
Tory II-C off-design performance
1963-04-22

This memorandum reports the performance of TORY II-C at off-design altitudes and Mach numbers. Inlet pressure recovery has been varied with Mach number, reasonable values for a real inlet having been chosen. Nozzle throat area and exit area have been fixed at the design values. Hence this study ...

DOE Information Bridge

17
High Reynolds Number, Low Mach Number, Steady Flow ...
1987-12-01

... The steady state cases investigated are at .3 Mach and Reynolds numbers of 1 to 5 million and at .12 Mach and a Reynolds number of 1.5 million. ...

DTIC Science & Technology

18
Far Wake Behind Cylinders at Hypersonic Speeds: Ii. stability.
1967-01-01

At Reynolds numbers below 10,000 the inner viscous wake behind cylinders at Mach 6 is entirely laminar. At these low Reynolds numbers the outer wake caused by the bow shock becomes transitional thousands of diameters downstream. Flowfield measurements (Pa...

National Technical Information Service (NTIS)

19
COSMOLOGY, MACH'S PRINCIPLE AND RELATIVITY,
1963-07-01

... Accession Number : AD0415787. Title : COSMOLOGY, MACH'S PRINCIPLE AND RELATIVITY,. Corporate Author : PRINCETON ...

DTIC Science & Technology

20
Skin Friction Measurements at a Mach Number of Three and ...
1980-09-01

... Title : Skin Friction Measurements at a Mach Number of Three and Momentum Thickness Reynolds Numbers Up to a Half Million. ...

DTIC Science & Technology

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21
EFFECT OF MACH NUMBER ON STREAMWISE VORTICES ...
1965-07-01

... Accession Number : AD0623460. Title : EFFECT OF MACH NUMBER ON STREAMWISE VORTICES IN LAMINAR REATTACHING FLOWS. ...

DTIC Science & Technology

22
5 - NASA Technical Reports Server

Mar 1, 2011 ... The variation of lift-curve slope with Mach number was gradual with a ... The drag rise begins at a Mach number of 0.90, and at Mach number ...

NASA Website

23
Accretion Disk Evolution with Wind Infall II. Results of 3D Hydrodynamical Simulations with an Illustrative Application to

the disk. That is, the gas was assumed to be highly supersonic. Figure 7 shows the averaged Mach number for the infalling wind as it impacts the disk. On average, the gas is indeed supersonic, but, particularly.--- Plot of the Mach number, averaged over OE and the two sides of the disk, of the gas impacting

E-print Network

24
Accretion Disk Evolution with Wind Infall II. Results of 3D Hydrodynamical Simulations with an Illustrative Application to

. Figure 7 shows the averaged Mach number for the infalling wind as it impacts the disk. On average . #12; { 11 { Fig. 7.| Plot of the Mach number, averaged over #30; and the two sides of the disk, of the gas for the two runs are strongly correlated. Thus, the average rate of mass falling onto the disk is ...

E-print Network

25
Calculating Mach Numbers Using Ratios and Fractions
2004-01-01

A mach number represents how many times the speed of sound a vehicle is traveling. NASA uses mach numbers to describe the speed of their planes. This video shows you how algebra can be used to determine the mach number of a NASA plane.

NSDL National Science Digital Library

26
Mach 10/14 Operations in the NSWC Hypervelocity Wind Tunnel Number 9 (Vertical Heater Vessel Leg).
1982-01-01

The original design of the Tunnel No. 9 Hypervelocity Facility called for three distinct Mach number capabilities; namely Mach 10, Mach 15, and Mach 20. The Mach 15 (now Mach 14) and Mach 10 legs are operational. However, problems ...

National Technical Information Service (NTIS)

27
Mach and Speed of Sound Applet - NASA

Sep 2, 2010... calculates the speed of sound and the mach number for an input velocity and altitude. Return to Mach number page, or speed of sound page. ...

NASA Website

28
DEVELOPMENT OF A VARIABLE MACH NUMBER SLIDING ...
1955-03-01

... Title : DEVELOPMENT OF A VARIABLE MACH NUMBER SLIDING BLOCK NOZZLE AND EVALUATION IN THE MACH 1.3 TO 4.0 RANGE. ...

DTIC Science & Technology

29
THE DESIGN AND OPERATION OF A HIGH MACH NUMBER ...
1968-12-01

... Title : THE DESIGN AND OPERATION OF A HIGH MACH NUMBER- REYNOLDS ... A running time of three seconds is available with the present ...

DTIC Science & Technology

30
SOME FLUTTER EXPERIMENTS AT A MACH NUMBER OF ...
1953-10-07

... SOME FLUTTER EXPERIMENTS AT A MACH NUMBER OF 1.3 ON CANTILEVER WINGS WITH TUBULAR AND CLOSED BODIES AT THE TIPS. ...

DTIC Science & Technology

31
NOSE BLUNTNESS, CONE ANGLE, AND MACH NUMBER ...
1967-09-01

... Title : NOSE BLUNTNESS, CONE ANGLE, AND MACH NUMBER EFFECTS ON THE STABILITY DERIVATIVES OF SLENDER CONES. ...

DTIC Science & Technology

32
Mach Number - Activity - NASA

The speed of sound depends on the composition and temperature of the air and it decreases with altitude. Use the definition of Mach number obtained from the ...

NASA Website

33
Low Mach number Euler computations
1989-01-01

Numerical solutions of the Euler equations for two-dimensional airfoil flows at low Mach numbers are

NASA Technical Reports Server (NTRS)

34
Critical Mach Numbers of Thin Airfoil Sections with Plain Flaps
1946-04-01

... Experimental observations show that the accuracy of this correction Is good for Mach numbers up through critical values. ...

DTIC Science & Technology

35
Chaotic behaviour of high Mach number flows
1985-01-01

The stability of the super-Alfvenic flow of a two-fluid plasma model with respect to the Mach number

NASA Technical Reports Server (NTRS)

36
Aerodynamic Performance and Turbulence Measurements in a ...

Mach numbers for three levels of turbulence. ... was to determine how the turbulence was affected by ... and Mach numbers, at different turbulence intensities. ...

NASA Website

37
AERODYNAMIC CHARACTERISTICS AT A MACH NUMBER ...
1958-08-04

... This report presents the r-sults of an investigation of the aerodynamic characteristics of these control arrangements at a Mach number of 6.8. ...

DTIC Science & Technology

38
A perforated-wall nozzle for variable Mach number testing.
1968-01-01

Perforated wall nozzle providing variable Mach number supersonic flow for external stream simulation

NASA Technical Reports Server (NTRS)

39
The Low Hub-Tip Ratio Supersonic Axial-Flow Compressor. Volume II.
1972-01-01

The report describes the test results of a supersonic axial-flow compressor stage with a tip Mach number of 2.0. This volume discusses a method to eliminate the inlet problem. (Author)

National Technical Information Service (NTIS)

40
TORY II- C PERFORMANCE PARAMETERS R. Var, P. M. Uthe, M. Mintz ...

Control tie rods (control rod fully withdrawn) . 3.64%. Side support structure . 7.4370. Page 4. Page 5. Flight Mach Number. Fig. ...

NASA Website

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41
Static Stability and Control Effectiveness of the Super HOBOS ...
1974-07-01

... Title : Static Stability and Control Effectiveness of the Super HOBOS/MK- 84 (EOGB-II) Munition at Mach Numbers from 0.4 to 1.6. ...

DTIC Science & Technology

42
NATIONAL ADVISORY COM-tiIi+Ei - NASA Technical Report Server (NTRS)

design lift raqe low-ayeed data do not suffice to Termit grcdiction of the Mach number at Tghich critical. caRressibility effecte occur- ...

NASA Website

43
An Improved Projectile Boattail. Part II
1976-03-01

... Projectiles With Anti-Magnus Vanes at Mach Numbers 0.7 Through 2.5," AEDC-TR-73-126; AFATL-TR-73-150; Propulsion Wind Tunnel Facility ...

DTIC Science & Technology

44
Airfoil Design and Rotorcraft Performance.
2002-01-01

The relationship between global performance of a typical helicopter and the airfoil environment, as represented by the airfoil angles of attack and Mach number, has been examined using the comprehensive analysis CAMRAD II. A general correspondence is obse...

National Technical Information Service (NTIS)

45
Aerodynamic tests of a Strypi II/NASA/ECHO at Mach numbers of 4. 98 and 7. 82 (Test VI-101)
1980-10-01

A Strypi II/NASA/ECHO model was tested in the Sandia 18-Inch Hypersonic Wind Tunnel to obtain six-component force data. Body-fin-rocket, body-fin, and body configurations were tested at Mach numbers of 4.98 and 7.82, three roll attitudes, (0, 45, and 90 degrees) and angles of attach from -6 to 8 degrees. All the data are presented in ...

Energy Citations Database

46
TABLES FOR CALCULATION OF REYNOLDS NUMBER AS A ...
1963-02-18

... Title : TABLES FOR CALCULATION OF REYNOLDS NUMBER AS A FUNCTION OF MACH NUMBER, STAGNATION PRESSURE, AND ...

DTIC Science & Technology

47
Results from Flight and Simulator Studies of a Mach 3 Cruise - NASA

Original Altitude and Mach Hold Control Systems . FLIGHT ... For subsonic jet transports , accurate control of altitude and Mach number is necessary for such ...

NASA Website

48
Turbulent Skin Friction at High Mach Numbers and Reynolds ...

... Accession Number : ADA397011. Title : Turbulent Skin Friction at High Mach Numbers and Reynolds Numbers in Air and Helium. ...

DTIC Science & Technology

49
Accuracy of the lattice Boltzmann method for describing the behavior of a gas in the continuum limit.
2010-11-15

The accuracy of the lattice Boltzmann method (LBM) for describing the behavior of a gas in the continuum limit is systematically investigated. The asymptotic analysis for small Knudsen numbers is carried out to derive the corresponding fluid-dynamics-type equations, and the errors of the LBM are estimated by comparing them with the correct fluid-dynamics-type equations. We ...

PubMed

50
Accuracy of the lattice Boltzmann method for describing the behavior of a gas in the continuum limit
2010-11-01

The accuracy of the lattice Boltzmann method (LBM) for describing the behavior of a gas in the continuum limit is systematically investigated. The asymptotic analysis for small Knudsen numbers is carried out to derive the corresponding fluid-dynamics-type equations, and the errors of the LBM are estimated by comparing them with the correct fluid-dynamics-type equations. We ...

NASA Astrophysics Data System (ADS)

51
Tabular and Grapical Solutions of Regular and Mach ...
1985-06-01

... FREEZING, SHOCK, GRAPHICS, FLOW, MACH NUMBER, CARBON DIOXIDE, WEDGES, ARGON, FLUORIDES, SULFUR COMPOUNDS. ...

DTIC Science & Technology

52
Quantitative Measures of the Mach-Dvorak Phenomenon with ...
1972-06-30

... Accession Number : AD0751180. Title : Quantitative Measures of the Mach-Dvorak Phenomenon with Asymmetrical Stimulation. ...

DTIC Science & Technology

53
PRESSURE DISTRIBUTIONS ON FLAT PLATES AT MACH 4 ...
1958-07-28

... Accession Number : AD0203699. Title : PRESSURE DISTRIBUTIONS ON FLAT PLATES AT MACH 4 AND LOW DENSITY FLOW. ...

DTIC Science & Technology

54
OPTIMUM SOURCE SIZE FOR THE MACH-ZEHNDER ...
1950-09-01

... Accession Number : AD0479435. Title : OPTIMUM SOURCE SIZE FOR THE MACH-ZEHNDER INTERFEROMETER,. Corporate ...

DTIC Science & Technology

55
Measurement of Pressure in Mach Reflection of Strong Shock ...
1972-06-01

... Accession Number : AD0746613. Title : Measurement of Pressure in Mach Reflection of Strong Shock Waves in a Shock Tube,. ...

DTIC Science & Technology

56
Magnetogasdynamic Flow Control of a Mach Reflection
2004-03-01

... Accession Number : ADA424159. Title : Magnetogasdynamic Flow Control of a Mach Reflection. Descriptive Note : Master's thesis. ...

DTIC Science & Technology

57
Mach Controller,
1975-01-03

... Accession Number : ADA006830. Title : Mach Controller,. Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO. ...

DTIC Science & Technology

58
LAMINAR HEAT TRANSFER TO A HEMISPHERE AT MACH ...
1956-02-20

... Title : LAMINAR HEAT TRANSFER TO A HEMISPHERE AT MACH NUMBER 3.2 AND AT LOW HEAT-TRANSFER RATES. ...

DTIC Science & Technology

59
Aerodynamic characteristics of lenticular and elliptic shaped configurations at a mach number of 6
1965-01-01

Aerodynamic characteristics of lenticular and elliptic shaped lifting-reentry configurations at Mach

NASA Technical Reports Server (NTRS)

60
A MACH-ZEHNDER INTERFEROMETER FOR SHOCK TUBE ...
1955-05-20

... Accession Number : AD0079595. Title : A MACH-ZEHNDER INTERFEROMETER FOR SHOCK TUBE APPLICATIONS. Corporate ...

DTIC Science & Technology

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61
Study of Altitude and Mach Number Effects on Exhaust Gas ...
1971-12-01

... Accession Number : AD0741249. Title : Study of Altitude and Mach Number Effects on Exhaust Gas Emissions of an Afterburning Turbofan Engine. ...

DTIC Science & Technology

62
Similarity Solution for Low Mach Number Spherical Shocks
1988-10-01

... Accession Number : ADA203285. Title : Similarity Solution for Low Mach Number Spherical Shocks. Corporate Author : NAVAL ...

DTIC Science & Technology

63
Shock-Wave Boundary Layer Interactions
1986-02-01

... the wall Mach number distributions relative to different Reynolds numbers R 6 , the initial Mach number Mo and shape parameter Rio being the ...

DTIC Science & Technology

64
High Angle of Attack Missile Aerodynamics at Mach Numbers ...
1980-11-01

... of both surface pressures and total forces and moments were made at a variety of Mach numbers and Reynolds number combinations. ...

DTIC Science & Technology

65
Effect of Mach and Reynolds Numbers on Maximum Lift ...
1946-03-01

... Accession Number : ADA801364. Title : Effect of Mach and Reynolds Numbers on Maximum Lift Coefficient. Descriptive Note : Technical note. ...

DTIC Science & Technology

66
Effect of Mach Number on Slender Vehicle Dynamics.
1981-01-01

... Accession Number : ADD521235. Title : Effect of Mach Number on Slender Vehicle Dynamics. Descriptive Note : Journal article,. ...

DTIC Science & Technology

67
Aerodynamics of Tactical Weapons to Mach Number 8 and ...
1981-05-01

... Accession Number : ADD523918. Title : Aerodynamics of Tactical Weapons to Mach Number 8 and Angle of Attack of 180 Degrees. ...

DTIC Science & Technology

68
Acoustic Computations for a Low Mach Number Heated ...
1994-01-01

... CD Drag coefficient plete acoustic formulation, for ... MN Mach number Navier-Stokes equations. ... Nu Nusselt number tional Fluid Dynamics (CFD ...

DTIC Science & Technology

69
PART I. DYNAMICAL SIMILARITY AND PART II. INTRINSIC RELATIONS IN MAGNETOHYDRODYNAMICS. Technical Summary Report
1961-09-01

A discussion is presented on the constancy and similarities of dynamics such as: magnetic Reynolds number, magnetic Mach number, the ratio of the viscous and magnetic diffusivities, Hartman number and various combinations of these values. In addition, an analysis is made of some of the intrinsic equations of ...

Energy Citations Database

70
Design of a High Reynolds Number Mach Number 8 ...
1972-08-01

... numbers. (Author). Descriptors : *HYPERSONIC NOZZLES, *HYPERSONIC WIND TUNNELS, HYPERSONIC NOZZLES, REYNOLDS NUMBER, ...

DTIC Science & Technology

71
Role of Whistler Oscillations in the Formation of the Structure of High Mach Number Collisionless Shock.
1989-01-01

It is shown that critical Mach number formation of the structure of the front of collisionless shock is concerned with nonlinear solitary wave packet of whistler oscillations. This critical Mach number is not the same as usually defined when ohmic dissipa...

National Technical Information Service (NTIS)

73
Absolute/Convective Instabilities and the Convective Mach Number in a Compressible Mixing Layer.
1989-01-01

Two aspects of the stability of a compressible mixing layer: Absolute/Convective instability and the convective Mach number were considered. It was shown that, for Mach numbers less than one, the compressible mixing layer is convectively unstable unless t...

National Technical Information Service (NTIS)

74
Physical properties of jets in low-luminosity radio sources
1990-05-01

The results of fitting Bicknell's semiempirical turbulent jet model to a sample of 23 jets taken from the B2 extragalactic radio sources studied in detail using the VLA are presented. It is found that the model fits are generally very reasonable and that the single most important parameter in the fits is the ratio of galaxy virial temperature to interstellar medium temperature. In most ...

Energy Citations Database

75
Aerodynamic Loads and Separation Characteristics from the F-4C for the MGGB MK-II Guided Weapon at Mach Numbers 0.7 to 1.3.
1974-01-01

Wind tunnel tests were conducted using 0.05-scale models to study the aerodynamic loads and separation characteristics from the F-4C aircraft for the MGGB MK-II store. The aerodynamic characteristics of the store were determined at free-stream conditions ...

National Technical Information Service (NTIS)

76
Variable Mach Number Wall Jets for Control/Propulsion on ...

... Title : Variable Mach Number Wall Jets for Control/Propulsion on Hypervelocity Projectiles/Interceptors: Tests with an Existing Model. ...

DTIC Science & Technology

77
THRUST AUGMENTATION IN AN UNSTEADY SUPERSONIC EJECTOR

Thrust augmentation results for a primary flow Mach number of 3.7, secondary flow Mach numbers ... they affect the thrust augmentation of a pulsed ejector. ...

NASA Website

78
TABLES FOR DETERMINATION OF FLOW VARIABLE ...
1960-01-01

... of Mach number and shock wave slope, from which the following are ... study of flow of a reLaxing ges behind shock waves at large Mach numbers. ...

DTIC Science & Technology

79
Some experimental studies of panel flutter at Mach number 1.3
1957-01-01

Experimental studies of panel flutter using thin metal plates were conducted at a Mach number of 1.3

NASA Technical Reports Server (NTRS)

80
Sidewall Mach Number Distributions for the NASA Langley Transonic ...

butterfly valve anda gatevalve allowing fastermodelconfigurationchanges;5) a ... the flap shapes for various Mach number ranges with a table of the re-entry ...

NASA Website

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81
Shock Wave Structure in Gas-Particle Mixtures at Low Mach ...
1981-07-01

... Accession Number : ADP000289. Title : Shock Wave Structure in Gas-Particle Mixtures at Low Mach Numbers,. Corporate ...

DTIC Science & Technology

82
Shock Wave - NASA Technical Report Server (NTRS)

area change are analyzed in terms of the incident shock wave. Mach number ... shock wave, measured by the shock wave Mach number, and the area ratio ...

NASA Website

83
STUDY OF FLOW OVER OSCILLATING AIRFOIL MODELS AT ...
1961-12-01

... AT A MACH NUMBER OF 7.0 IN HELIUM By Ali Arman ... AT A MACH NUMBER OF 7.0 IN HELIUM By Ali Arman SUMMARY ...

DTIC Science & Technology

84
Pressure test on the Viking lander capsule at Mach number 10
1972-01-01

Surface pressure tests were made on a scale model of the Viking Lander Capsule at Mach number 10 and

NASA Technical Reports Server (NTRS)

85
Pressure Losses in Simple Dump Combustors
1972-10-01

... Personal Author(s) : Barclay, Lewis P. ... problems can lead to serious errors at Mach numbers above 0.3 ... loss as a function of the Mach number and a ...

DTIC Science & Technology

86
Operational Experience in the Mach Number 10-20 Range in ...
1959-09-01

... Title : Operational Experience in the Mach Number 10-20 Range in the Princeton University Helium Hypersonic Wind Tunnel,. ...

DTIC Science & Technology

87
Mach Number - Teacher - Glenn Research Center - NASA

Jul 14, 2008 ... After reading an explanation from a NASA Web-based textbook, you will demonstrate your understanding of Mach numbers by using them to ...

NASA Website

88
Mach Number - NASA

Mar 16, 2010 ... The Mach number M allows us to define flow regimes in which ... The Space Shuttle re-enters the atmosphere at high hypersonic speeds, ...

NASA Website

89
Mach Number - NASA

Jan 13, 2006 ... But a sharp disturbance generates a shock wave that affects both the lift ... The Mach number M allows us to define flight regimes in which ...

NASA Website

90
Investigation of Wing Characteristics at a Mach Number of ...
1948-06-21

... Title : Investigation of Wing Characteristics at a Mach Number of 1.53. 3 - Unswept Wings of Differing Aspect Ratio and Taper Ratio. ...

DTIC Science & Technology

91
Frequency dependence of coherent structures in a Mach number 0.6 jet
1984-01-01

The existence of a large scale structure in a Mach number 0.6, axisymmetric jet of cold air has been

NASA Technical Reports Server (NTRS)

92
FLIGHT-DETERMINED AERODYNAMIC-NOISE ...
1962-03-01

... AIRPLANE NOSE CONE UP TO A MACH NUMBER OF 2 By Norman J. McLeod ... AIRPLANE NOSE CONE UP TO A MACH NUMBER OF 2 H ...

DTIC Science & Technology

93
Experimental boundary-layer edge mach numbers for two space shuttle

The results show that the Mach number at the edge of the boundary layer is .... entropy moving rearward on the body), and the thickness at a given station ...

NASA Website

94
Efficient Large-Eddy Simulations of Low Mach Number Flows ...
2001-08-01

... In practice, most multigrid applications are for steady state problems. ... For low Mach number flows, the efficiency of nsiltigrid strongly depends on the ...

DTIC Science & Technology

95
Effects of Independent Variations of Mach Number and ...
1952-11-01

... The section lift characteristics were determined for Mach numbers ranging from ... x 10(exp 6) to 9.0 x 10(exp 6). For the airfoil sections with abrupt ...

DTIC Science & Technology

96
Effect of Various Parameters Including Mach Number on the ...
1951-12-01

... Title : Effect of Various Parameters Including Mach Number on the Single-Degree-of-Freedom Flutter of a Control Surface in Potential Flow. ...

DTIC Science & Technology

97
Effect of Mach Number on the Maximum Lift and Buffeting ...
1947-06-12

... Title : Effect of Mach Number on the Maximum Lift and Buffeting Boundary Determined in Flight on a North American P-51D Airplane. ...

DTIC Science & Technology

98
Critical Mach Numbers of Circulation Control Airfoils as ...
1972-08-01

... Title : Critical Mach Numbers of Circulation Control Airfoils as Determined by Finite-Difference Methods. Descriptive Note : Technical note,. ...

DTIC Science & Technology

99
Characteristics of Perforated Diffusers at Free-Stream Mach ...
1950-05-08

... Accession Number : ADA801298. Title : Characteristics of Perforated Diffusers at Free-Stream Mach Number 1.90. Descriptive ...

DTIC Science & Technology

100
Aerodynamics of Tactical Weapons to Mach Number 3 and ...
1977-02-01

... to compute the lift, drag, pitching moment, magnus moment, roll damping moment, and pitch damping moment ... Mach number 3 and angle of attack ...

DTIC Science & Technology

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101
AN EXAMPLE OF ONE-DIMENSIONAL GAS FLOW WITH ...
1959-09-10

... An example concerning the heat transfer and pressure drop ... inlet Mach number on pressure loss, exit Mach number and total area required to ...

DTIC Science & Technology

102
AERODYNAMICS OF SLENDER BODIES AT MACH ...
1954-05-06

... Title : AERODYNAMICS OF SLENDER BODIES AT MACH NUMBER OF 3.12 AND REYNOLDS NUMBERS FROM 2X106 TO 15X106. ...

DTIC Science & Technology

103
A Study of Rectangular Supersonic Jets Modified for Mixing ...
2001-06-30

... of high Reynolds and Mach numbers flows such ... nozzle, and the jet Mach number were explored. ... were also performed on a Hartmann Tube based ...

DTIC Science & Technology

104
A Simplified Chart for Determining Mach Number and True ...
1943-03-01

... for Determining Mach Number and True Airspeed from Airspeed-Indicator Readings AUTHOR|S ... SUBJECT HEADINGS: Airspeed indicators (09700) ...

DTIC Science & Technology

105
A Simplified Chart for Determining Mach Number and True ...
1943-03-01

... Collection includes both citations and many full-text, downloadable documents ... Title : A Simplified Chart for Determining Mach Number and True ...

DTIC Science & Technology

106
8 - NASA Technical Reports Server

Mar 1, 2011 ... The variation of lift-curve slope with Mach number was gradual with a ... a value of 62 percent mean aerodynamic chord at a Mach number of ...

NASA Website

107
.Low Mach Number Euler Computations NASA

for incompressible potential flow. The purpose of the present study is to assess the accuracy of an Euler code at low Mach number and to investigate the factors ...

NASA Website

108
(Design and Calibration of the X-33 Flush Airdata Sensing ... - NASA

surface incidence angle. To blend the two solutions over. a large range of Mach numbers, ...... Mach number and the local incidence angles; thus for a ...

NASA Website

109
Enhanced Combustion Pulsejet Engine (ECPE) for Mach 0 to 3 ...

1995 Phase II. Enhanced Combustion Pulsejet Engine (ECPE) for Mach 0 to 3 Applications ... Enhanced Combustion Pulsejet Engine on Target Drone ...

NASA Website

110
Mach Number Dependence of Electron Heating in High Mach Number Quasiperpendicular Shocks
2010-03-12

Efficiency of electron heating through microinstabilities generated in the transition region of a quasi-perpendicular shock for wide ange of Mach numbers is investigated by utilizing PIC (Particle-In-Cell) simulation and model analyses. In the model analyses saturation levels of effective electron temperature as a result of microinstabilities are estimated ...

E-print Network

111
The sooner you can get high fidelity data The better off you are ...

No matter what the stage of your aerothermodynamic design project, ... which makes the Mach 10 tunnel ideally suited for heat transfer studies. ... Mach 6 High Temperature Air Tunnel the effects of Mach number, Reynolds number, ...

NASA Website

112
PRELIMINARY STUDIES OF THE FLOW AROUND TWO ...
1966-01-01

... Accession Number : AD0631474. ... AROUND TWO-DIMENSIONAL BODIES AT HIGH MACH NUMBERS AND LOW REYNOLDS NUMBERS. ...

DTIC Science & Technology

113
Evaluation of Reynolds Number and Tunnel Wall Porosity ...
1976-07-01

... Title : Evaluation of Reynolds Number and Tunnel Wall Porosity Effects on Nozzle Afterbody Drag at Transonic Mach Numbers. ...

DTIC Science & Technology

114
EFFECT OF REYNOLDS NUMBER ON TURBINE ...
1964-03-13

... Title : EFFECT OF REYNOLDS NUMBER ON TURBINE PERFORMANCE AT VARIOUS MACH NUMBERS. Descriptive Note : Final rept.,. ...

DTIC Science & Technology

115
An Investigaion of Boattail Geometry and Reynolds Number ...
1977-02-01

... Title : An Investigaion of Boattail Geometry and Reynolds Number Effects on Forebody and Afterbody Drag at Transonic Mach Numbers. ...

DTIC Science & Technology

116
Three dimensional supersonic flows with subsonic axial Mach numbers
1976-01-01

A numerical approach is presented for the computation of flows in which the component of velocity in

NASA Technical Reports Server (NTRS)

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