Experimental Investigation Of Base Pressure On Blunt Trailing Edge Wings At Supersonic Velocities

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Experimental Investigation Of Base Pressure On Blunt Trailing Edge Wings At Supersonic Velocities

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Author : Dean R. Chapman
language : en
Publisher:
Release Date : 1952

Experimental Investigation Of Base Pressure On Blunt Trailing Edge Wings At Supersonic Velocities written by Dean R. Chapman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with Aerodynamics, Supersonic categories.

The pressres acting on the base of blunt-trailing-edge airfoils have been measured at Mach numbers of 1.25, 1.5, 2.0, and 3.1 and at Reynolds numbers from 0.2 to 3.8 million. Data are presented for 29 profiles both with laminar and with turbulent boundary layers approaching the trailing edges of the wings. The base pressure is found to be a function primarily of Mach number and the ratio of the boundary layer thickeness at the trailing edge to the trailing-edge thickness.

Experimental Investigation Base Pressure On Blunt Trailing Edge Wings At Supersonic Velocities

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Author : Dean R. Chapman
language : en
Publisher:
Release Date : 1952

Experimental Investigation Base Pressure On Blunt Trailing Edge Wings At Supersonic Velocities written by Dean R. Chapman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with Aerodynamics, Supersonic categories.

The pressres acting on the base of blunt-trailing-edge airfoils have been measured at Mach numbers of 1.25, 1.5, 2.0, and 3.1 and at Reynolds numbers from 0.2 to 3.8 million. Data are presented for 29 profiles both with laminar and with turbulent boundary layers approaching the trailing edges of the wings. The base pressure is found to be a function primarily of Mach number and the ratio of the boundary layer thickeness at the trailing edge to the trailing-edge thickness.

Technical Note National Advisory Committee For Aeronautics

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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1956

Technical Note National Advisory Committee For Aeronautics written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Aeronautics categories.

Nasa Technical Note

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Author :
language : en
Publisher:
Release Date : 1973

Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with categories.

Report

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Author :
language : en
Publisher:
Release Date : 1957

Report written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aeronautics categories.

Report

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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1958

Report written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with Aeronautics categories.

Annual Report Of The National Advisory Committee For Aeronautics

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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1948

Annual Report Of The National Advisory Committee For Aeronautics written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1948 with Aeronautics categories.

Includes the Committee's Reports no. 1-1058, reprinted in v. 1-37.

Aerodynamics Of Guided And Unguided Weapons

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Author : Frankie Gale Moore
language : en
Publisher:
Release Date : 1973

Aerodynamics Of Guided And Unguided Weapons written by Frankie Gale Moore and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with Guided missiles categories.

Several theoretical and empirical procedures are combined into a single computer program to predict lift, drag, and center of pressure on quite general wing-body geometries. The method is applicable for Mach number zero to three and angle-of-attack zero to about fifteen degrees. Computed results for several configurations compare well with experimental and other analytical results. It costs about five dollars per Mach number to compute the static aerodynamics of a typical wing-body shape on the CDC 6700 computer.

Technical Note

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Author :
language : en
Publisher:
Release Date : 1952

Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with Aeronautics categories.

Research Abstracts

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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1951

Research Abstracts written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1951 with Aeronautics categories.