Dryden Technical Report Server
From the NTRS FAQ: Where do I go for a hardcopy of the report?
- EVALUATION OF VARIOUS THRUST CALCULATION TECHNIQUES ON AN F404 ENGINE , Technical Paper
Authors: Ronald J. Ray
Report Number: NASA-TP-3001
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Format(s) on-line:
PDF (1,745 KBytes)
Report Date: April 1990
No. Pages: 31
- THE EFFECTIVENESS OF VANE-AILERON EXCITATION IN THE EXPERIMENTAL DETERMINATION OF FLUTTER SPEED BY PARAMETER IDENTIFICATION , Technical Paper
Authors: E. Nissim
Report Number: NASA-TP-2971
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Format(s) on-line:
PDF (900 KBytes)
Report Date: January 1990
No. Pages: 24
- OPTIMUM ELEMENT DENSITY STUDIES FOR FINITE-ELEMENT THERMAL ANALYSIS OF HYPERSONICAIRCRAFT STRUCTURES , Technical Memorandum
Authors: William L. Ko, Timothy Olona and Kyle M. Muramoto
Report Number: NASA-TM-4163
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Format(s) on-line:
PDF (1,391 KBytes)
Report Date: January 1990
No. Pages: 36
- OUTPUT MODEL-FOLLOWING CONTROL SYNTHESIS FOR AN OBLIQUE-WING AIRCRAFT , Technical Memorandum
Authors: Joseph W. Pahle
Report Number: NASA-TM-100454
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Format(s) on-line:
PDF (926 KBytes)
Report Date: April 1990
No. Pages: 30
- EFFECTS OF WING SWEEP ON BOUNDARY-LAYER TRANSITIONFOR A SMOOTH F-14A WING AT MACH NUMBERS FROM 0.700 TO0.825 , Technical Memorandum
Authors: Bianca Trujillo Anderson and Robert R. Meyer, Jr.
Report Number: NASA-TM-101712
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Format(s) on-line:
PDF (2,330 KBytes)
Report Date: May 1990
No. Pages: 48
- EXPERIMENTAL CHARACTERIZATION OF THE EFFECTS OF PNEUMATIC TUBING ON UNSTEADY PRESSUREMEASUREMENTS , Technical Memorandum
Authors: Stephen A. Whitmore, William T. Lindsey, Robert E. Curry and Glenn B. Gilyard
Report Number: NASA-TM-4171
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (1,118 KBytes)
Report Date: March 1990
No. Pages: 31
- WIND-TUNNEL INVESTIGATION OF A FLUSH AIRDATA SYSTEM AT MACH NUMBERS FROM 0.7 TO 1.4 , Technical Memorandum
Authors: Terry J. Larson, Timothy R. Moes and Paul M. Siemers, III
Report Number: NASA-TM-101697
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (1,514 KBytes)
Report Date: April 1990
No. Pages: 35
- DESIGN OF CONTROL LAWS FOR FLUTTER SUPPRESSION BASED ON THE AERODYNAMIC ENERGY CONCEPT AND COMPARISONS WITH OTHER DESIGN METHODS , Technical Paper
Authors: Eli Nissim (Technion - Israel Inst. of Tech.)
Report Number: NASA-TP-3056
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Format(s) on-line:
PDF (2,069 KBytes)
Report Date: October 1990
No. Pages: 59
- FLIGHT CHARACTERISTICS OF A MODIFIED SCHWEIZER SGS 1-36 SAILPLANE AT LOW AND VERY HIGH ANGLES OF ATTACK , Technical Paper
Authors: Alex G. Sim
Report Number: NASA-TP-3022
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Format(s) on-line:
PDF (1,497 KBytes)
Report Date: July 1990
No. Pages: 48
- EFFECTS OF WING SWEEP ON IN-FLIGHT BOUNDARY-LAYERTRANSITION FOR A LAMINAR FLOW WING AT MACH NUMBERS FROM 0.60TO 0.79 , Technical Memorandum
Authors: Bianca Trujillo Anderson and Robert R. Meyer, Jr.
Report Number: NASA-TM-101701
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (1,777 KBytes)
Report Date: July 1990
No. Pages: 37
- OPEN-MODE DELAMINATION STRESS CONCENTRATIONS IN HORSESHOE AND ELLIPTIC COMPOSITE CURVED BARS SUBJECTED TO END FORCES , Technical Memorandum
Authors: William L. Ko and Raymond H. Jackson
Report Number: NASA-TM-4164
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (813 KBytes)
Report Date: January 1990
No. Pages: 25
- WATER-TUNNEL STUDY RESULTS OF A TF/A-18 AND F/A-18 CANOPY FLOW VISUALIZATION , Technical Memorandum
Authors: Steven A. Johnson and David F. Fisher
Report Number: NASA-TM-101705
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Currently this document is not available on-line.
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Report Date: March 1990
No. Pages: 29
- IN-FLIGHT INVESTIGATION OF SHUTTLE TILE PRESSURE ORIFICE INSTALLATIONS , Technical Memorandum
Authors: Timothy R. Moes and Robert R. Meyer, Jr.
Report Number: NASA-TM-4219
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (1,826 KBytes)
Report Date: September 1990
No. Pages: 38
- IN-FLIGHT FLOW VISUALIZATION CHARACTERISTICS OF THE NASA F-18 HIGH ALPHA RESEARCH VEHICLE AT HIGHANGLES OF ATTACK , Technical Memorandum
Authors: David F. Fisher, John H. Del Frate and David M. Richwine
Report Number: NASA-TM-4193
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (10,950 KBytes)
Report Date: May 1990
No. Pages: 34
- AIRDATA CALIBRATION OF A HIGH-PERFORMANCE AIRCRAFT FOR MEASURING ATMOSPHERIC WINDPROFILES , Technical Memorandum
Authors: Edward A. Haering, Jr.
Report Number: NASA-TM-101714
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Format(s) on-line:
PDF (1,261 KBytes)
Report Date: January 1990
No. Pages: 27
- PRELIMINARY RESULTS FROM A SUBSONIC HIGH ANGLE-OF-ATTACK FLUSH AIRDATA SENSING (HI-FADS)SYSTEM: DESIGN, CALIBRATION, AND FLIGHT TEST EVALUATION , Technical Memorandum
Authors: Stephen A. Whitmore, Timothy R. Moes and Terry J. Larson
Report Number: NASA-TM-101713
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (976 KBytes)
Report Date: January 1990
No. Pages: 13
- COMPENSATING FOR PNEUMATIC DISTORTION IN PRESSURE SENSING DEVICES , Technical Memorandum
Authors: Stephen A. Whitmore and Cornelius T. Leondes
Report Number: NASA-TM-101716
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (979 KBytes)
Report Date: January 1990
No. Pages: 21
- AN IN-FLIGHT INTERACTION OF THE X-29A CANARD AND FLIGHT CONTROL SYSTEM , Technical Memorandum
Authors: Michael W. Kehoe , Edward J. Laurie and Lisa J. Bjarke
Report Number: NASA-TM-101718
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Currently this document is not available on-line.
From the NTRS FAQ: Where do I go for a hardcopy of the report?
Report Date: April 1990
No. Pages: 21
- IN-FLIGHT FLOW FIELD ANALYSIS ON THE NASA F-18 HIGH ALPHA RESEARCH VEHICLE WITHCOMPARISONS TO GROUND FACILITY DATA , Conference Paper
Authors: John H. Del Frate and Fanny A. Zuniga
Report Number: H-1592
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Currently this document is not available on-line.
From the NTRS FAQ: Where do I go for a hardcopy of the report?
Report Date: January 1990
No. Pages: 27
- AN AUTOMATED CALIBRATION LABORATORY FOR FLIGHTRESEARCH INSTRUMENTATION: REQUIREMENTS AND APROPOSED DESIGN APPROACH , Technical Memorandum
Authors: Nora Oneill-Rood and Richard D. Glover
Report Number: NASA-TM-101719
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (1,321 KBytes)
Report Date: May 1990
No. Pages: 16
- OVERVIEW OF THE NASA AMES-DRYDEN INTEGRATED TEST FACILITY , Conference Paper
Authors: Dale Mackall, David Mcbride and Dorothea Cohen
Report Number: NASA-TM-101720
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Format(s) on-line:
PDF (1,284 KBytes)
Report Date: May 1990
No. Pages: 15
- EFFECTS OF SIMPLIFYING ASSUMPTIONS ON OPTIMAL TRAJECTORY ESTIMATION FOR A HIGH-PERFORMANCE AIRCRAFT , Technical Memorandum
Authors: Lura E. Kern (NASA Ames Research Center), Steve D. Belle (PRC Systems Services Co.) and Eugene L. Duke (NASA Hugh L. Dryden Flight Research Facility)
Report Number: NASA-TM-101721
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (852 KBytes)
Report Date: April 1990
No. Pages: 27
- FLUTTER CLEARANCE OF THE F-14A VARIABLE-SWEEPTRANSITION FLIGHT EXPERIMENT AIRPLANE, PHASE 2 , Technical Memorandum
Authors: Lawrence C. Freudinger and Michael W. Kehoe
Report Number: NASA-TM-101717
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (1,080 KBytes)
Report Date: July 1990
No. Pages: 43
- REAL-TIME AERODYNAMIC HEATING AND SURFACE TEMPERATURE CALCULATIONS FOR HYPERSONIC FLIGHT SIMULATION , Technical Memorandum
Authors: Robert D. Quinn and Leslie Gong
Report Number: NASA-TM-4222
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (1,182 KBytes)
Report Date: August 1990
No. Pages: 44
- PROPULSION SYSTEM-FLIGHT CONTROL INTEGRATION ANDOPTIMIZATION: FLIGHT EVALUATION AND TECHNOLOGY TRANSITION , Technical Memorandum
Authors: Frank W. Burcham, Jr., Glenn B. Gilyard and Lawrence P. Myers
Report Number: NASA-TM-4207
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (1,304 KBytes)
Report Date: July 1990
No. Pages: 26
- A PRELIMINARY EVALUATION OF AN F100 ENGINE PARAMETER ESTIMATION PROCESS USING FLIGHT DATA , Technical Memorandum
Authors: Trindel A. Maine, Glenn B. Gilyard and Heather H. Lambert
Report Number: NASA-TM-4216
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (1,325 KBytes)
Report Date: August 1990
No. Pages: 32
- PREDICTED AND MEASURED IN-FLIGHT WING DEFORMATIONSOF A FORWARD-SWEPT-WING AIRCRAFT , Conference Paper
Authors: William A. Lokos
Report Number: H-1612
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Currently this document is not available on-line.
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Report Date: January 1990
No. Pages: 20
- FLIGHT TEST OF A TRAJECTORY CONTROLLER USING LINEARIZINGTRANSFORMATIONS WITH MEASUREMENT FEEDBACK , Conference Paper
Authors: Robert F. Antoniewicz (NASA Hugh L. Dryden Flight Research Facility), Eugene L. Duke (NASA Flight Research Center) and P. K. A. Menon (Georgia Institute of Technology)
Report Number: H-1619
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Currently this document is not available on-line.
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Report Date: January 1990
No. Pages: 15
- ESTIMATING SHORT-PERIOD DYNAMICS USING ANEXTENDED KALMAN FILTER , Technical Memorandum
Authors: Jeffrey E. Bauer (NASA Ames Research Center) and Dominick Andrisani (Purdue University)
Report Number: NASA-TM-101722
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (1,213 KBytes)
Report Date: January 1990
No. Pages: 38
- A PRELIMINARY EVALUATION OF AN F100 ENGINE PARAMETER ESTIMATION PROCESS USING FLIGHT DATA
Authors: Trindel A. Maine, Glenn B. Gilyard and Heather H. Lambert
Report Number: NASA-TM-4216
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (1,382 KBytes)
Report Date: August 1990
No. Pages: 29
- FLIGHT CONTROL SYSTEM DESIGN FACTORS FOR APPLYING AUTOMATED TESTING TECHNIQUES , Technical Memorandum
Authors: Joel R. Sitz (NASA Hugh L. Dryden Flight Research Facility) and Todd H. Vernon (Planning Research Corp.)
Report Number: NASA-TM-4242
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (1,179 KBytes)
Report Date: October 1990
No. Pages: 17
- VALIDATION OF THE F-18 HIGH ALPHA RESEARCH VEHICLE FLIGHT CONTROL AND AVIONICS SYSTEMS MODIFICATIONS , Technical Memorandum
Authors: Vince Chacon, Joseph W. Pahle and Victoria A. Regenie
Report Number: NASA-TM-101723
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (865 KBytes)
Report Date: October 1990
No. Pages: 13
- F-18 HIGH ALPHA RESEARCH VEHICLE SURFACE PRESSURES:INITIAL IN-FLIGHT RESULTS AND CORRELATION WITH FLOW VISUALIZATIONAND WIND-TUNNEL DATA , Technical Memorandum
Authors: David F. Fisher, Daniel W. Banks and David M. Richwine
Report Number: NASA-TM-101724
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (2,772 KBytes)
Report Date: August 1990
No. Pages: 36
- FLIGHT-TESTING OF THE SELF-REPAIRING FLIGHT CONTROL SYSTEM USING THE F-15 HIGHLY INTEGRATED DIGITAL ELECTRONIC CONTROL FLIGHT RESEARCH FACILITY , Technical Memorandum
Authors: James F. Stewart and Thomas L. Shuck
Report Number: NASA-TM-101725
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (734 KBytes)
Report Date: August 1990
No. Pages: 17
- A PROPOSED KALMAN FILTER ALGORITHM FOR ESTIMATION OFUNMEASURED OUTPUT VARIABLES FOR AN F100 TURBOFAN ENGINE , Technical Memorandum
Authors: Gurbux S. Alag (PRC Systems Services Co.) and Glenn B. Gilyard (NASA Hugh L. Dryden Flight Research Facility)
Report Number: NASA-TM-4234
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (1,108 KBytes)
Report Date: October 1990
No. Pages: 32
- REAL-TIME APPLICATION OF ADVANCED THREE-DIMENSIONAL GRAPHIC TECHNIQUES FOR RESEARCH AIRCRAFT SIMULATION , Technical Memorandum
Authors: Steven B. Davis
Report Number: NASA-TM-101730
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (1,198 KBytes)
Report Date: December 1990
No. Pages: 21
- A SIMPLE DYNAMIC ENGINE MODEL FOR USE IN A REAL-TIMEAIRCRAFT SIMULATION WITH THRUST VECTORING , Technical Memorandum
Authors: Steven A. Johnson
Report Number: NASA-TM-4240
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (978 KBytes)
Report Date: October 1990
No. Pages: 21
- IN-FLIGHT FLOW VISUALIZATION WITH PRESSURE MEASUREMENTS AT LOW SPEEDS ON THE NASA F-18 HIGH ALPHA RESEARCH VEHICLE , Technical Memorandum
Authors: John H. Delfrate, David F. Fisher and Fanny A. Zuniga
Report Number: NASA-TM-101726
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (3,812 KBytes)
Report Date: October 1990
No. Pages: 45
- TECHNIQUES FOR HOT STRUCTURES TESTING , Technical Memorandum
Authors: V. Michael Deangelis and Roger A. Fields
Report Number: NASA-TM-101727
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (1,755 KBytes)
Report Date: November 1990
No. Pages: 28
- INTEGRATED FLIGHT-PROPULSION CONTROL CONCEPTS FOR SUPERSONIC TRANSPORT AIRPLANES , Technical Memorandum
Authors: Frank W. Burcham, Jr., Glenn B. Gilyard and Paul A. Gelhausen
Report Number: NASA-TM-101728
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (1,055 KBytes)
Report Date: November 1990
No. Pages: 18
- A PRELIMINARY LOOK AT TECHNIQUES USED TO OBTAINAIRDATA FROM FLIGHT AT HIGH ANGLES OF ATTACK , Technical Memorandum
Authors: Timothy R. Moes and Stephen A. Whitmore
Report Number: NASA-TM-101729
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (2,178 KBytes)
Report Date: December 1990
No. Pages: 51
- MONITORING TECHNIQUES FOR THE X-29A AIRCRAFT'SHIGH-SPEED ROTATING POWER TAKEOFF SHAFT , Technical Memorandum
Authors: David F. Voracek
Report Number: NASA-TM-101731
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
Availability:
Format(s) on-line:
PDF (925 KBytes)
Report Date: December 1990
No. Pages: 25
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