A Study of Several Theoretical Methods for Computing the Zero-lift Wave Drag of a Family of Open-nosed Bodies of Revolution in the Mach Number Range of 2.0 to 4.0
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Presley, Leroy L↗
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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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An Investigation of Supersonic Turbulent Boundary Layers on Slender Bodies of Revolution in Free Flight by Use of a Mach-zehnder Interferometer and Shadowgraphs
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Seiff, Alvin↗
Preliminary Heat-transfer Studies on Two Bodies of Revolution at Angle of Attack at a Mach Number of 3.12
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Sands, Norman↗
Experimental Investigation of the Effects of Support Interference on the Drag of Bodies of Revolution at a Mach Number of 1.5
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Perkins, Edward W↗
: the Linear Perturbation Theory of Axially Symmetric Compressible Flow with Application to the Effect of Compressibility on the Pressure Coefficient at the Surface of a Body of Revolution
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Herriot, John G↗
Effect of Number of Fins on the Drag of a Pointed Body of Revolution at Low Supersonic Velocities
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Mastrocola, N↗
Experimental Investigation of the Effects of Viscosity on the Drag of Bodies of Revolution at a Mach Number 1.5
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Chapman, Dean R↗
The calculation of drag for airfoil sections and bodies of revolution at subcritical speeds
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Heaslet, Max A↗
Pressure Distribution over a Sharp-nose Body of Revolution at Transonic Speeds by the NACA Wing-flow Method
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Danforth, Edward C B↗
A comparison of the experimental subsonic pressure distributions about several bodies of revolution with pressure distributions computed by means of the linearized theory
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Matthews, Clarence W↗
Error in airspeed measurement due to static-pressure field ahead of sharp-nose bodies of revolution at transonic speeds
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Danforth, Edward C↗
Estimation of the forces and moments acting on inclined bodies of revolution of high fineness ratio
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Allen, H Julian↗
Aerodynamic Investigation of a Parabolic Body of Revolution at Mach Number of 1.92 and Some Effects of an Annular Jet Exhausting from the Base
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Love, Eugene S↗
Flight Investigation at High-subsonic, Transonic, and Supersonic Speeds to Determine Zero-lift Drag of Bodies of Revolution Having Fineness Ratio of 6.04 and Varying Positions of Maximum Diameter
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Katz, Ellis R↗
Measurements of the Drag and Pressure Distribution on a Body of Revolution Throughout Transition from Subsonic to Supersonic Speeds
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Thompson, Jim Rogers↗
Flight measurements of drag and base pressure of a fin-stabilized parabolic body of revolution (NACA RM-10) at different Reynolds numbers and at Mach numbers from 0.9 to 3.3
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Jackson, H Herbert↗
Flight investigation at Mach numbers from 0.8 to 1.5 to determine the effects of nose bluntness on the total drag of two fin-stabilized bodies of revolution
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Hart, Roger G↗
Average Skin-friction Coefficients from Boundary-layer Measurements in Flight on a Parabolic Body of Revolution (NACA RM-10) at Supersonic Speeds and at Large Reynolds Numbers
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Rumsey, Charles B↗