The Effects of Reynolds Number at Mach Numbers up to 0.94 on the Loading on a 35 Degree Swept-back Wing Having NACA 65(1)A012 Streamwise Sections
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Tinling, Bruce E↗
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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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Drag of Circular Cylinders for a Wide Range of Reynolds Numbers and Mach Numbers
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Gowen, Forrest E↗
Investigation of the variation with Reynolds number of the base, wave, and skin-friction drag of a parabolic body of revolution (NACA RM-10) at Mach numbers of 1.62, 1.93, and 2.41 in the Langley 9-inch supersonic tunnel
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Love, Eugene S↗
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↗
Aerodynamic characteristics of two delta wings at Mach number 4.04 and correlations of lift and minimum-drag data for delta wings at Mach numbers from 1.62 to 6.9
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Ulmann, Edward F↗
Effect of Variations in Reynolds Number on the Aerodynamic Characteristics of Three Bomb or Store Shapes at a Mach Number of 1.62 with and Without Fins
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Rainey, Robert W↗
Aerodynamics of Slender Bodies at Mach Number of 3.12 and Reynolds Numbers from 2 x 10(exp 6) to 15 x 10(exp 6) III : Boundary Layer and Force Measurements on a Slender Cone-cylinder Body of Revolution
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Jack, John R↗
Experimental Investigation of the Effects of Support Interference on the Pressure Distribution of a Body of Revolution at a Mach Number of 3.12 and Reynolds Numbers from 2 x 10(exp 6) to 14 x 10(exp 6)
A compilation of available information on the problem of support interference at transonic and supersonic speeds is presented. (author)
Baughman, L Eugene↗
Investigation of Reynolds Number Effects for a Series of Cone-cylinder Bodies at Mach Numbers of 1.62, 1.93, and 2.41
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Ogburn, Edmund L↗
Aerodynamic Characteristics of a 68.4 Degree Delta Wing at Mach Numbers of 1.6 and 1.9 over a Wide Reynolds Number Range
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Hatch, John E , Jr↗
Measurements and Predictions of Flow Conditions on a Two-dimensional Base Separating a Mach Number 3.36 Jet and a Mach Number 1.55 Outer Stream
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Coletti, Donald E↗
An Investigation of the Effects of Jet Exhaust and Reynolds Number upon the Flow over the Vertical Stabilizer and Rudder of the Douglas D-558-II Research Airplane at Mach Numbers of 1.62, 1.93, and 2.41
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Grigsby, Carl E↗
Drag and Heat Transfer on a Parabolic Body of Revolution (NACA RM-10) in Free Flight to Mach Number 2 with Both Constant and Varying Reynolds Number and Heating Effects on Turbulent Skin Friction
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Maloney, Joseph P↗
Investigation of the lift, center of pressure, and drag of a projectile at a Mach number of 8.6 and a Reynolds number of 17 million
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Canning, Thomas N↗
Comparison of experimental and theoretical normal-force distributions (including Reynolds number effects) on an ogive-cylinder body at Mach number 1.98
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Perkins, Edward W↗
Effects of leading-edge radius on the longitudinal stability of two 45 degree sweptback wings as influenced by Reynolds numbers up to 8.20 x 10(exp 6) and Mach numbers up to 0.303
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Foster, Gerald V↗
Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration
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Rumsey, Charles B↗
Free-flight Tests to Determine the Power-on and Power-off Pressure Distribution and Drag of the NACA RM-10 Research Vehicle at Large Reynolds Numbers Between Mach Numbers 0.8 and 3.0
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Hoffman, Sherwood↗