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- SOME CORRELATIONS OF FLIGHT-MEASURED AND WIND-TUNNEL MEASURED STABILITY AND CONTROL CHARACTERISTICS OF HIGH-SPEED AIRPLANES
Authors: Walter C. Williams, Hubert M. Drake and Jack Fischel
Report Number: NACA-H56AG62
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: August 1956
No. Pages: 20
- SKIN AND STRUCTRUAL TEMPERATURE MEASUREMENTS ON RESEARCH AIRPLANES AT SUPERSONIC SPEEDS
Authors: Richard D. Banner and Frank S. Malvestuto, Jr.
Report Number: NACA-H56BANN
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: October 1956
No. Pages: 13
- FLIGHT EXPERIENCE WITH PRESENT RESEARCH AIRPLANES
Authors: Hubert M. Drake
Report Number: NACA-H56DRAK
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: October 1956
No. Pages: 9
- GENERAL BACKGROUND OF THE X-15 RESEARCH-AIRPLANE PROJECT
Authors: Dr. Hugh L. Dryden
Report Number: NACA-H56DRYD
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: October 1956
No. Pages: 6
- STUDIES OF REACTION CONTROLS
Authors: Wendell H. Stillwell
Report Number: NACA-H56STIL
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: October 1956
No. Pages: 8
- INSTRUMENTATION FOR THE X-15
Authors: I. Taback and G.M. Truszynski
Report Number: NACA-H56TABA
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: October 1956
No. Pages: 11
- AN ANALOG STUDY OF THE RELATIVE IMPORTANCE OF VARIOUS FACTORS AFFECTING ROLL COUPLING
Authors: Joseph Weil and Richard E. Day
Report Number: NACA-RM-H56A06
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: April 1956
No. Pages: 82
- FLIGHT MEASUREMENTS OF HORIZONTAL-TAIL LOADS ON THE DOUGLAS X-3 RESEARCH AIRPLANE
Authors: Harriet J. Stephenson
Report Number: NACA-RM-H56A23
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: April 1956
No. Pages: 34
- TIME-VECTOR DETERMINED LATERAL DERIVATIVES OF A SWEPT-WING FIGHTER-TYPE AIRPLANE WITH THREE DIFFERENT VERTICAL TAILS AT MACH NUMBERS BETWEEN 0.70 AND1.48
Authors: Cheste H. Wolowicz
Report Number: NACA-RM-H56C20
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: June 1956
No. Pages: 95
- FLIGHT DETERMINATION OF THE LATERAL HANDLING QUALITIES OF THE BELL X-5 RESEARCH AIRPLANE AT 58.7 DEGREES SWEEPBACK
Authors: Thomas W. Finch and Joseph A. Walker
Report Number: NACA-RM-H56C29
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: May 1956
No. Pages: 42
- EFFECT OF SEVERAL WING MODIFICATIONS ON THE SUBSONIC AND TRANSONIC LONGITUDINAL HANDLING QUALITIES OF THE DOUGLAS D-558-II RESEARCH AIRPLANE
Authors: Jack Fischel and Donald Reisert
Report Number: NACA-RM-H56C30
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: June 1956
No. Pages: 60
- LIFT AND DRAG OF THE BELL X-5 RESEARCH AIRPLANE IN THE 45 DEGREE SWEPTBACK CONFIGURATION AT TRANSONIC SPEEDS
Authors: Jack Nugent
Report Number: NACA-RM-H56E02
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: July 1956
No. Pages: 24
- FLIGHT-DETERMINED TRANSONIC LIFT AND DRAG CHARACTEISTICS OF THE YF-102 AIRPLANE WITH TWO WING CONFIGURATIONS
Authors: Edwin J. Saltzman, Donald R. Bellman and Norman T. Musialowski
Report Number: NACA-RM-H56E08
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: July 1956
No. Pages: 45
- CORRELATION OF FLIGHT AND ANALOG INVESTIGATIONS OF ROLL COUPLING
Authors: Joseph Weil and Richard E. Day
Report Number: NACA-RM-H56F08
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: September 1956
No. Pages: 20
- FLIGHT EVALUATION OF THE LATERAL STABILITY AND CONTROL CHARACTERISTICS OF THE CONVAIR YF-102 AIRPLANE
Authors: Thomas R. Sisk, William H. Andrews and Robert W. Darville
Report Number: NACA-RM-H56G11
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: January 1956
No. Pages: 39
- WING LOADS AND LOAD DISTRIBUTIONS THROUGHOUT THE LIFT RANGE OF THE DOUGLAS X-3 RESEARCH AIRPLANE AT TRANSONIC SPEEDS
Authors: Earl R. Keener and Gareth H. Jordan
Report Number: NACA-RM-H56G13
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: November 1956
No. Pages: 192
- DYNAMIC LONGITUDINAL STABILITY CHARACTERISTICS OF A SWEPT-WING FIGHTER-TYPE AIRPLANE AT MACH NUMBERS BETWEEN 0.36 AND 1.45
Authors: Chester H. Wolowicz
Report Number: NACA-RM-H56H03
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: April 1956
No. Pages: 29
- ANALYSIS OF THE VERTICAL-TAIL LOADS MEASURED DURING A FLIGHT INVESTIGATION AT TRANSONIC SPEEDS OF THE DOUGLAS X-3 RESEARCH AIRLANE
Authors: William L. Marcy, Harriet J. Stephenson and Thomas V. Cooney
Report Number: NACA-RM-H56H08
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: November 1956
No. Pages: 33
- LONGITUDINAL STABILITY CHARACTERISTICS OF THE CONVAIR YF-102 AIRPLANE DETERNINED FROM FLIGHT TESTS
Authors: William H. Andrews, Thomas R. Sisk and Robert W. Darville
Report Number: NACA-RM-H56I17
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: January 1956
No. Pages: 41
- AN ANALYSIS OF ESTIMATED AND EXPERIMENTAL TRANSONIC DOWNWASH CHARACTERISTICS AS AFFECTED BY PLAN FORM AND THICKNESS FOR WING AND WING-FUSELAGE CONFIGURATIONS.
Authors: Joseph Weil, George S. Campbell and Margaret S. Diederich
Report Number: NACA-TN-3628
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: April 1956
- FLIGHT TECHNIQUES FOR DETERMINING AIRPLANE DRAG AT HIGH MACH NUMBERS
Authors: De E. Beeler, Donald R. Bellmen and Edwin J. Saltzman
Report Number: NACA-TN-3821
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: August 1956
No. Pages: 41
- COMPARISON OF FLIGHT AND WIND-TUNNEL MEASUREMENTS OF HIGH-SPEED-AIRPLANE STABILITY AND CONTROL CHARACTERISTICS
Authors: Walte C. Williams, Hubert M. Drake and Jack Fischel
Report Number: NACA-TN-3859
Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
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Report Date: August 1956
No. Pages: 17
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