Dryden Technical Report Server
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- AEROELASTIC EFFECTS OF AERODYNAMIC HEATING
Authors: Hugh L. Dryden and Dr. John E. Duberg
Report Number: AGARD20-P10
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: June 1955
No. Pages: 10
- FLIGHT EXPERIENCE OF INERTIA COUPLING IN ROLLING MANEUVERS
Authors: Joseph Weil, Ordway B. Gates, Jr., Richard D. Banner and Albert E. Kuhl
Report Number: NACA-H55WEIL
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: March 1955
No. Pages: 12
- ROLLING PERFORMANCE OF THE REPUBLIC YF-84F AIRPLANE AS MEASURED IN FLIGHT , Research Memorandum
Authors: John B. McKay
Report Number: NACA-RM-H54G20A
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: January 1955
- FLIGHT MEASUREMENTS OF ELEVON HINGE MOMENTS ON THE XF-92A DELTA-WING AIRPLANE , Research Memorandum
Authors: Clinton T. Johnson and Albert E. Kuhl
Report Number: NACA-RM-H54J25A
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: January 1955
- FLIGHT MEASUREMENTS OF THE DYNAMIC LONGITUDINAL STABILITY AND FREQUENCY-RESPONSE CHARACTERISTICS OF THE XF-92A DELTA-WING AIRPLANE , Research Memorandum
Authors: Euclid C. Holleman and William C. Triplett
Report Number: NACA-RM-H54J26A
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: January 1955
- LONGITUDINAL STABILITY CHARACTERISTICS IN MANEUVERING FLIGHT OF THE CONVAIR XF-92A DELTA-WING AIRPLANE INCLUDING THE EFFECTS OF WING FENCES , Research Memorandum
Authors: Thomas R. Sisk and Duane O. Muhleman
Report Number: NACA-RM-H54J27
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: January 1955
- THE EFFECT OF THE BLUNT-TRAILING-EDGE ELEVONS ON THE LONGITUDINAL AND LATERAL HANDLING QUALITIES OF THE X-4 SEMITAILLESS AIRPLANE , Research Memorandum
Authors: Edwin J. Saltzman
Report Number: NACA-RM-H54K03
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: January 1955
- RESULTS OF MEASUREMENTS MADE DURING THE APPROACH AND LANDING OF SEVEN HIGH-SPEED RESEARCH AIRPLANES
Authors: Wendell H. Stillwell
Report Number: NACA-RM-H54K24
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: February 1955
No. Pages: 25
- FLIGHT MEASUREMENTS AT TRANSONIC SPEEDS OF THE BUFFETING CHARACTERISTICS OF THE XF-92A DELTA-WING RESEARCH AIRPLANE , Research Memorandum
Authors: Thomas F. Baker and Wallace E. Johnson
Report Number: NACA-RM-H54L03
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: April 1955
- WING-LOAD MEASUREMENTS AT SUPERSONIC SPEEDS OF THE DOUGLAS D-558-II RESEARCH AIRPLANE , Research Memorandum
Authors: Glenn H. Robinson, George E. Cothren and Chris Pembo
Report Number: NACA-RM-H54L27
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: March 1955
- FLIGHT-DETERMINED PRESSURE DISTRIBUTIONS OVER A SECTION OF THE 35 DEGREE SWEPT WING OF THE DOUGLAS D-558-II RESEARCH AIRPLANE AT MACH NUMBERS UP TO 2.0
Authors: Gareth H. Jordan and Earl R. Keener
Report Number: NACA-RM-H55A03
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: January 1955
No. Pages: 38
- PRELIMINARY FLIGHT-DETERMINED PRESSURE DISTRIBUTIONS OVER THE WING OF THE DOUGLAS X-3 RESEARCH AIRPLANE AT SUBSONIC AND TRANSONIC MACH NUMBERS
Authors: Gareth H. Jordan and C. Kenneth Hutchins, Jr.
Report Number: NACA-RM-H55A10
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: April 1955
No. Pages: 35
- WING-LOAD MEASUREMENTS OF THE BELL X-5 RESEARCH AIRPLANE AT A SWEEP ANGLE OF 58.70
Authors: Richard D. Banner, Robert D. Reed and William L. Marcy
Report Number: NACA-RM-H55A11
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: April 1955
No. Pages: 23
- FLIGHT EXPERIENCE WITH TWO HIGH-SPEED AIRPLANES HAVING VIOLENT LATERAL-LONGITUDINAL COUPLING IN AILERON ROLLS
Authors: Staff
Report Number: NACA-RM-H55A13
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: February 1955
No. Pages: 33
- LATERAL STABILITY AND CONTROL CHARACTERISTICS OF THE CONVAIR XF-92 DELTA-WING AIRPLANE AS MEASURED IN FLIGHT
Authors: Thomas R. Sisk and Duane O. Muhleman
Report Number: NACA-RM-H55A17
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: May 1955
No. Pages: 56
- FLIGHT DETERMINATION OF THE LONGITUDINAL STABILITY AND CONTROL CHARACTERISTICS OF THE BELL X-5 RESERCH AIRPLANE AT 58.7 DEGREES SWEEPBACK
Authors: Thomas W. Finch
Report Number: NACA-RM-H55C07
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: May 1955
No. Pages: 31
- FLIGHT MEASUREMENTS OF WING LOADS ON THE CONVAIR XF-92A DELTA-WING AIRPLANE
Authors: Albert E. Kuhl and Clinton T. Johnson
Report Number: NACA-RM-H55D12
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: May 1955
No. Pages: 35
- STABILITY AND CONTROL CHARACTERISTICS OBTAINED DURING DEMONSTRATION OF THE DOUGLAS X-3 RESEARCH AIRPLANE
Authors: Richard E. Day and Jack Fischel
Report Number: NACA-RM-H55E16
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: July 1955
No. Pages: 52
- FLIGHT EXPERIENCE OF INERTIA COUPLING IN ROLLING MANEUVERS
Authors: Joseph Weil, Ordway B. Gates, Jr., Richard D. Banner and Albert E. Kuhl
Report Number: NACA-RM-H55E17B
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: July 1955
No. Pages: 13
- FLIGHT MEASUREMENTS OF HORIZONTAL-TAIL LOADS ON THE BELL X-5 RESEARCH AIRPLANE AT A SWEEP ANGLE OF 58.7 DEGREES
Authors: Robert D. Reed
Report Number: NACA-RM-H55E20A
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: July 1955
No. Pages: 20
- FLIGHT MEASUREMENTS OF THE LATERAL RESPONSE CHARACTERISTICS OF THE CONVAIR XF-92A DELTA-WING AIRPLANE
Authors: Euclid C. Holleman
Report Number: NACA-RM-H55E26
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: August 1955
No. Pages: 38
- EFFECT OF SEVERAL WING MODIFICATIONS ON THE LOW-SPEED STALLING CHARACTERISTICS OF THE DOUGLAS D-558-II RESEARCH AIRPLANE
Authors: Jack Fischel and Donald Reisert
Report Number: NACA-RM-H55E31A
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: July 1955
No. Pages: 63
- WING PRESSURE DISTRIBUTIONS OVER THE LIFT RANGE OF THE CONVAIR XF-92A DELTA-WING AIRPLANE AT SUBSONIC AND TRANSONIC SPEEDS
Authors: Earl R. Keener and Gareth H. Jordan
Report Number: NACA-RM-H55G07
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: November 1955
No. Pages: 135
- BEHAVIOR OF THE BELL X-1A RESEARCH AIRPLANE DURING EXPLORATORY FLIGHTS AT MACH NUMBERS NEAR 2.0 AND AT EXTREME ALTITUDES
Authors: Hubert M. Drake and Wendell H. Stillwell
Report Number: NACA-RM-H55G25
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: September 1955
No. Pages: 25
- FLIGHT MEASUREMENTS OF DIRECTIONAL STABILITY TO A MACH NUMBER OF 1.48 FOR AN AIRPLANE TESTED WITH THREE DIFFERENT VERTICAL TAIL CONFIGURATIONS
Authors: Hubert M. Drake, Thomas W. Finch and James R. Peele
Report Number: NACA-RM-H55G26
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Postscript (4,463 KBytes)
PDF (878 KBytes)
Report Date: January 1955
No. Pages: 24
- FLIGHT EXPERIENCE WITH A DELTA-WING AIRPLANE HAVING VIOLENT LATERAL-LONGITUDINAL COUPLING IN AILERON ROLLS
Authors: Thomas R. Sisk and William H. Andrews
Report Number: NACA-RM-H55H03
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: October 1955
No. Pages: 19
- FLIGHT MEASUREMENTS OF THE DYNAMIC LATERAL AND LONGITUDINAL STABILITY OF THE BELL X-5 RESEARCH AIRPLANE AT 58.7 DEGREES SWEEPBACK
Authors: Edward N. Videan
Report Number: NACA-RM-H55H10
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: October 1955
No. Pages: 70
- FLIGHT MEASUREMENTS OF THE VERTICAL-TAIL LOADS ON THE CONVAIR XF-92A DELTA-WING AIRPLANE
Authors: Clinton T. Johnson
Report Number: NACA-RM-H55H25
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: October 1955
No. Pages: 24
- MACH NUMBER MEASUREMENTS AND CALIBRATIONS DURING FLIGHT AT HIGH SPEEDS AND AT HIGH ALTITUDES INCLUDING DATA FOR THE D-558-II RESEARCH AIRPLANE
Authors: Cyril D. Brunn and Wendell H. Stillwell
Report Number: NACA-RM-H55J18
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Postscript (1,295 KBytes)
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Report Date: March 1955
No. Pages: 32
- FLIGHT INVESTIGATION OF THE EFFECT OF VERTICAL-TAIL SIZE ON THE ROLLING BEHAVIOR OF A SWEPT-WING AIRPLANE HAVING LATERAL-LONGITUDINAL COUPLING
Authors: Thomas W. Finch, James R. Peele and Richard E. Day
Report Number: NACA-RM-H55L28A
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: April 1955
No. Pages: 34
- SOME RECENT RESEARCH ON THE HANDLING QUALITIES OF AIRPLANES
Authors: Walter C. Williams and William H. Phillips
Report Number: NACA-RM-H55L29A
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: February 1955
No. Pages: 20
- FLIGHT CALIBRATION OF FOUR AIRSPEED SYSTEMS ON A SWEPT-WING AIRPLANE AT MACH NUMBERS UP TO 1.04 BY THE NACA RADAR-PHOTOTHEODOLITE METHOD
Authors: Jim Rogers Thompson, Richard S. Bray and George E. Cooper
Report Number: NACA-TN-3526
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Postscript (4,080 KBytes)
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Report Date: November 1955
No. Pages: 37
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