Dryden Technical Report Server
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- ANALYSIS OF LONGITUDINAL PILOT-INDUCED OSCILLATION TENDENCIES OF YF-12 AIRCRAFT , Technical Note
Authors: J. W. Smith and D. T. Berry
Report Number: NASA-TN-D-7900
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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From the NTRS FAQ: Where do I go for a hardcopy of the report?
Report Date: February 1975
No. Pages: 40
- A NEW FLIGHT TEST DATA SYSTEM FOR NASA AERONAUTICAL FLIGHT RESEARCH , Conference Paper
Authors: K. C. Sanderson
Report Number: H-833
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: January 1975
No. Pages: 17
- HIGH ALTITUDE GUST ACCELERATION ENVIRONMENT AS EXPERIENCED BY A SUPERSONIC AIRPLANE , Technical Note
Authors: L. J. Ehernberger and B. J. Love
Report Number: NASA-TN-D-7868
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: January 1975
No. Pages: 26
- MECHANIZATION OF AND EXPERIENCE WITH A TRIPLEX FLY-BY-WIRE BACKUP CONTROL SYSTEM
Authors: W. P. Lock, W. R. Petersen and G. B. Whitman
Report Number: H-839
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: February 1975
No. Pages: 31
- FLIGHT TEST EXPERIENCE WITH THE F-8 DIGITAL FLY-BY-WIRE SYSTEM
Authors: K. J. Szalai
Report Number: H-840
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: February 1975
No. Pages: 54
- DESIGN AND DEVELOPMENT EXPERIENCE WITH A DIGITAL FLY-BY-WIRE CONTROLSYSTEM IN AN F-8C AIRPLANE
Authors: D. A. Deets
Report Number: H-841
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: February 1975
No. Pages: 28
- FLIGHT DETERMINED LIFT AND DRAG CHARACTERISTICS OF AN F-8 AIRPLANE MODIFIED WITH A SUPERCRITICAL WING WITH COMPARISON TO WIND-TUNNEL RESULTS , Technical Memorandum
Authors: J. S. Pyle and L. L. Steers
Report Number: NASA-TM-X-3250
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: June 1975
No. Pages: 87
- AN OVERVIEW OF NASA'S DIGITAL FLY-BY-WIRE TECHNOLOGY DEVELOPMENTPROGRAM
Authors: C. R. Jarvis
Report Number: H-845
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: February 1975
No. Pages: 11
- A PILOT'S OPINION OF THE F-8 DIGITAL FLY-BY-WIRE AIRPLANE
Authors: G. E. Krier
Report Number: H-846
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: February 1975
No. Pages: 15
- EFFECTS OF TIME-SHIFTED DATA ON FLIGHT DETERMINED STABILITY AND CONTROL DERIVATIVES , Technical Note
Authors: S. T. Steers and K. W. Iliff
Report Number: NASA-TN-D-7830
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: March 1975
No. Pages: 86
- FLIGHT EVALUATION OF THE M2-F3 LIFTING BODY HANDLING QUALITIES AT MACH NUMBERS FROM 0.30 TO 1.61 , Technical Note
Authors: R. W. Kempel, W. H. Dana and A. G. Sim
Report Number: NASA-TN-D-8027
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: July 1975
No. Pages: 45
- DESCRIPTION AND FLIGHT TEST RESULTS OF THE NASA F-8 DIGITAL FLY-BY-WIRE CONTROL SYSTEM , Technical Note
Authors: Various
Report Number: NASA-TN-D-7843
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: February 1975
No. Pages: 198
- DEVELOPMENT OF A REMOTE DIGITAL AUGMENTATION SYSTEM AND APPLICATION TO A REMOTELY PILOTED RESEARCH VEHICLE , Technical Note
Authors: J. W. Edwards and D. A. Deets
Report Number: NASA-TN-D-7941
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: April 1975
No. Pages: 54
- AN ALGORITHM AND COMPUTER PROGRAM TO LOCATE REAL ZEROS OF REAL POLYNOMIALS , Technical Note
Authors: D. R. Hedgley, Jr.
Report Number: NASA-TN-D-8009
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: June 1975
No. Pages: 24
- A FORTRAN PROGRAM FOR DETERMINING AIRCRAFT STABILITY AND CONTROL DERIVATIVES FROM FLIGHT DATA , Technical Note
Authors: R. E. Maine and K. W. Iliff
Report Number: NASA-TN-D-7831
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: April 1975
No. Pages: 177
- EVALUATION OF A HEMISPHERICAL HEAD FLOW DIRECTION SENSOR FOR INLET DUCT MEASUREMENTS , Technical Memorandum
Authors: D. L. Bennett
Report Number: NASA-TM-X-3232
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: May 1975
No. Pages: 24
- MEASUREMENTS AND ANALYSIS OF AIRCRAFT AIRFRAME NOISE , Conference Paper
Authors: T. W. Putnam, P. L. Lasagna and K. C. White
Report Number: H-863
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: March 1975
No. Pages: 8
- AERODYNAMIC DRAG REDUCTION TESTS ON A FULL-SCALE TRACTOR-TRAILER COMBINATION AND A REPRESENTATIVE BOX-SHAPED GROUND VEHICLE , Conference Paper
Authors: L. L. Steers, L. C. Montoya and E. J. Saltzman
Report Number: H-875
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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From the NTRS FAQ: Where do I go for a hardcopy of the report?
Report Date: August 1975
No. Pages: 15
- EXPLORATORY WIND TUNNEL TESTS OF A SHOCK-SWALLOWING AIR DATA SENSOR AT A MACH NUMBER OF APPROXIMATELY 1.83 , Technical Memorandum
Authors: J. Nugent, L. M. Couch and L. D. Webb
Report Number: NASA-TM-X-56030
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: March 1975
No. Pages: 41
- A FLIGHT TEST INVESTIGATION OF THE ROLLING MOMENTS INDUCED ON A T-37B AIRPLANE IN THE WAKE OF A B-747 AIRPLANE , Technical Memorandum
Authors: H. J. Smith
Report Number: NASA-TM-X-56031
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: April 1975
No. Pages: 23
- COMPARISONS OF WING PRESSURE DISTRIBUTION FROM FLIGHT TESTS OF FLUSH AND EXTERNAL ORIFICES FOR MACH NUMBERS FROM 0.50 TO 0.97 , Technical Memorandum
Authors: L. C. Montoya and D. P. Lux
Report Number: NASA-TM-X-56032
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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PDF (876 KBytes)
Report Date: April 1975
No. Pages: 26
- STATUS OF A DIGITAL INTEGRATED PROPULSION/FLIGHT CONTROL SYSTEM FOR THE YF-12 AIRPLANE , Conference Paper
Authors: P. J. Reukauf, F. W. Burcham, Jr. and J. K. Holzman
Report Number: H-891
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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From the NTRS FAQ: Where do I go for a hardcopy of the report?
Report Date: September 1975
No. Pages: 9
- TECHNIQUES FOR DETERMINING PROPULSION SYSTEM FORCES FOR ACCURATE HIGH SPEED VEHICLE DRAG MEASUREMENTS IN FLIGHT , Conference Paper
Authors: H. H. Arnaiz
Report Number: H-893
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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From the NTRS FAQ: Where do I go for a hardcopy of the report?
Report Date: August 1975
No. Pages: 14
- REVIEW OF AIRCRAFT NOISE PROPAGATION , Technical Memorandum
Authors: T. W. Putnam
Report Number: NASA-TM-X-56033
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: September 1975
No. Pages: 60
- RESULTS OF NASTRAN MODAL ANALYSES AND GROUND VIBRATION TESTS ON THE YF-12A AIRPLANE , Conference Paper
Authors: E. E. Kordes and A. R. Curtis
Report Number: H-897
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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From the NTRS FAQ: Where do I go for a hardcopy of the report?
Report Date: November 1975
No. Pages: 25
- FLIGHT-DETERMINED STABILITY AND CONTROL DERIVATIVES FOR AN EXECUTIVE JET TRANSPORT , Technical Memorandum
Authors: H. J. Smith
Report Number: NASA-TM-X-56034
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: July 1975
No. Pages: 47
- STABILITY AND CONTROL DERIVATIVES OF THE T-37B AIRPLANE , Technical Memorandum
Authors: M. F. Shafer
Report Number: NASA-TM-X-56036
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: September 1975
No. Pages: 32
- MEASURED NOISE REDUCTIONS RESULTING FROM MODIFIED APPROACH PROCEDURES FOR BUSINESS JET AIRCRAFT , Technical Memorandum
Authors: F. W. Burcham, Jr., T. W. Putnam, P. L. Lasagna and O. O. Parish
Report Number: NASA-TM-X-56037
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: November 1975
No. Pages: 31
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