Related Books

The Effects of Aerodynamic Heating and Heat Transfer on the Surface Temperature of a Body of Revolution in Steady Supersonic Flight
Language: en
Pages: 542

The Effects of Aerodynamic Heating and Heat Transfer on the Surface Temperature of a Body of Revolution in Steady Supersonic Flight

Authors: Richard Scherrer
Categories: Aerodynamic heating
Type: BOOK - Published: 1947 - Publisher:

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An approximate method for determining the convective cooling requirement in the laminar-boundary-layer region of a body of revolution in high-speed flight was d
Report
Language: en
Pages: 30

Report

Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1951 - Publisher:

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Report - National Advisory Committee for Aeronautics
Language: en
Pages: 652

Report - National Advisory Committee for Aeronautics

Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1947 - Publisher:

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Annual Report of the National Advisory Committee for Aeronautics
Language: en
Pages: 664

Annual Report of the National Advisory Committee for Aeronautics

Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1951 - Publisher:

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Supersonic Wave Drag of Nonlifting Sweptback Tapered Wings with Mach Lines Behind the Line of Maximum Thickness
Language: en
Pages: 724

Supersonic Wave Drag of Nonlifting Sweptback Tapered Wings with Mach Lines Behind the Line of Maximum Thickness

Authors: Kenneth Margolis
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1948 - Publisher:

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Wave drag equations are derived for rhombic-profile tapered wings with maximum-thickness line swept less than the Mach line. Variations in drag with taper ratio