Average skin-friction drag coefficients from tank tests of a parabolic body of revolution (NACA RM-10)
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Loposer, J Dan↗
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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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Preliminary Investigation of the Effects of Heat Transfer on Boundary-layer Transition on a Parabolic Body of Revolution (NACA RM-10) at a Mach Number of 1.61
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FLOW, TURBULENT↗
An Extension of the Investigation of the Effects of Heat Transfer on Boundary-layer Transition on a Parabolic Body of Revolution (NACA RM-10) at a Mach Number of 1.61
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BODIES - SURFACE CONDITIONS↗
Theoretical investigation at subsonic speeds of the flow ahead of a slender inclined parabolic-arc body of revolution and correlation with experimental data obtained at low speeds
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Letko, William↗
On the small-disturbance iteration method for the flow of a compressible fluid with application to a parabolic cylinder
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Kaplan, Carl↗
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↗
Correlation of Supersonic Convective Heat-transfer Coefficients from Measurements of the Skin Temperature of a Parabolic Body of Revolution (NACA RM-10)
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Chauvin, Leo T↗
Pressure Distributions at Transonic Speeds for Parabolic-arc Bodies of Revolution Having Fineness Ratios of 10, 12, and 14
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Taylor, Robert A↗
Free-flight Investigation to Determine the Drag of Flat- and Vee- Windshield Canopies on a Parabolic Fuselage with and Without Transonic Indentation Between Mach Numbers of 0.75 and 1.35
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Kouyoumjian, Walter L↗
Flight Tests to Determine the Drag of Fin-stabilized Parabolic Bodies at Transonic and Supersonic Speeds
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Alexander, Sidney R↗
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 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↗
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↗
Correlation of Supersonic Convective Heat-transfer Coefficients from Measurements of the Skin Temperature of a Parabolic Body of Revolution (NACA RM-10)
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Chauvin, Leo T↗
Flight Determination of Drag and Pressure Recovery of a Nose Inlet of Parabolic Profile at Mach Numbers from 0.8 to 1.7
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Sears, Richard I↗
Flight Investigation at Mach Numbers from 0.8 to 1.5 of the Drag of a Canopy Located at Two Positions on a Parabolic Body of Revolution
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Welsh, Clement J↗
Base Pressures Measured on Several Parabolic-arc Bodies of Revolution in Free Flight at Mach Numbers from 0.8 to 1.4 and at Large Reynolds Numbers
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Katz, Ellis↗
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) : Body of Revolution with Near-parabolic Forebody and Cylindrical Afterbody
An experimental investigation of the aerodynamic characteristics of a slender, square-based body of revolution was conducted at a Mach number of 3.12 for angles of attack from 0 degree to 10 degrees and for Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6). Boundary-layer measurements at zero angle of attack are compared with several compressible flow formulating for predicting boundary-layer characteristics. Comparison of experimental pressure and force values with theoretical values showed good agreement for low angles of attack. The measured mean skin-friction coefficients agreed well with those predicted by Mangler's transformation for laminar flow over cones.
LOADS, AERODYNAMIC↗