Flight tests of a model having self-supporting fuel-carrying panels hinged to the wing tips
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Shanks, Robert E↗
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Results for “Flight tests”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Flight Tests to Determine the Effect of Taper on the Zero-lift Drag of Wings at Low Supersonic Speeds
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Alexander, Sidney R↗
Rocket-powered flight test of a roll-stabilized supersonic missile configuration
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Gardiner, Robert A↗
Results of flight tests to determine the zero-lift drag characteristics of a 60 degree delta wing with NACA 65-006 airfoil section and various double-wedge sections at Mach numbers from 0.7 to 1.6
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Welsh, Clement J↗
Transonic flight test to compare the zero-lift drag of underslung and symmetrical nacelles varied chordwise at 40 percent semispan of a 45 degree sweptback, tapered wing
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Pepper, William B , Jr↗
Investigation of the Dynamic Longitudinal Stability of Two Equal Size Models Coupled in Tandem with a Single Joint;Preliminary Model Flight Tests
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Shanks, Robert E↗
Some recent data from flight tests of rocket-powered models
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Comparison of Zero-lift Drags Determined by Flight Tests at Transonic Speeds of Symmetrically Mounted Nacelles in Various Spanwise Positions on a 45 Degrees Sweptback Wing and Body Combination
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Pepper, William B , Jr↗
Comparison of Zero-lift Drag Determined by Flight Tests at Transonic Speeds of Pylon, Underslung, and Symmetrically Mounted Nacelles at 40 Percent Semispan of a 45 Degrees Sweptback Wing and Body Combination
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Hoffman, Sherwood↗
Comparison of Zero-lift Drags Determined by Flight Tests at Transonic Speeds of Symmetrically Mounted Nacelles in Various Chordwise Positions at the Wing Tip of a 45 Degrees Sweptback Wing and Body Combination
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Pepper, William B , Jr↗
The Effect on Zero-lift Drag of an Indented Fuselage or a Thickened Wing-root Modification to a 45 Degrees Sweptback Wing-body Configuration as Determined by Flight Tests at Transonic Speeds
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Pepper, William B↗
Transonic Flight Tests to Determine Zero-lift Drag and Pressure Recovery of Nacelles Located at the Wing Tips on a 45 Degree Sweptback Wing and Body Combination
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Hoffman, Sherwood↗
Stability and Control Measurements Obtained During USAF-NACA Cooperative Flight-test Program on the X-4 Airplane (USAF No. 46-677)
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Ankenbruck, Herman O↗
Transonic Flight Tests to Compare the Zero-lift Drags of 45 Degree Sweptback Wings of Aspect Ratio 3.55 and 6.0 with and Without Nacelles at the Wing Tips
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Hoffman, Sherwood↗
Flutter of a 60 degree delta wing (NACA 65A003 airfoil) encountered at supersonic speeds during the flight test of a rocket-propelled model
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Judd, Joseph H↗
A Correlation with Flight Tests of Results Obtained from the Measurement of Wing Pressure Distributions on a 1/4-scale Model of the X-1 Airplane (10-percent-thick Wing)
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Runckel, Jack F↗
Results of Flight Tests to Determine the Drag of Finite-length Cylinders at High Reynolds Numbers for a Mach Number Range of 0.5 to 1.3
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Welsh, Clement J↗
Exploratory rocket flight tests to investigate the use of a freely spinning monoplane tail for stabilizing a body
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Purser, Paul E↗
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