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Correlation Of Wind Tunnel Blockage Data

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Correlation Of Wind Tunnel Blockage Data

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Author : Paul Czysz
language : en
Publisher:
Release Date : 1963

Correlation Of Wind Tunnel Blockage Data written by Paul Czysz and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Hypersonic wind tunnels categories.

An experimental investigation of the test section flow blockage characteristics was conducted at Mach 4 in the High Temperature Hypersonic Gas dynamics Facility. The models utilized in this program were pointed and blunted cones from 5 degree half angle to 90-degree half angle, flat plates, delta winged shapes, and hemispherical models, some of which were run up to 40-degree angle of attack. Comparison of the data with other facilities resulted in a correlation of the maximum model size compared to the potential flow core size with Mach number and drag coeffi cient for both open and closed test section con figurations for Mach numbers from 1.5 to greater than 10.

Correlation Of Wind Tunnel Blockage Data

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Author : Paul Czysz
language : en
Publisher:
Release Date : 1963

Nasa Technical Memorandum

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Author :
language : en
Publisher:
Release Date : 1989

Nasa Technical Memorandum written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with Aeronautics categories.

V Stol Wind Tunnel Testing

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Author :
language : en
Publisher:
Release Date : 1984

V Stol Wind Tunnel Testing written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1984 with categories.

Scientific And Technical Aerospace Reports

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Author :
language : en
Publisher:
Release Date : 1995

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995 with Aeronautics categories.

The High Temperature Hypersonic Gasdynamics Facility

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Author : Paul Czysz
language : en
Publisher:
Release Date : 1963

The High Temperature Hypersonic Gasdynamics Facility written by Paul Czysz and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Hypersonic wind tunnels categories.

The High Temperature, Hypersonic Gasdynamics Facility was developed as a result of the efforts of the Aeronautical Systems Division to extend the state-of-the art in hypersonic aerodynamics simulation. The High Temperature Facility is an operational hypersonic wind tunnel supplied by high pressure, heated air from a zirconium oxide pebble heater. The maximum stagnation pressure is 40 atmospheres, and the maximum temperature is 4700 R. The facility is one of four of its kind in this hemisphere and the only Air Force facility of its type. This report describes its operation from August 1961 until May 1962 as a Mach 4 aerodynamic test facility. The successful operation of this facility is a significant achievement in the area of hypersonic aero dynamic testing techniques.

Wind Tunnel Wall Interference January 1980 May 1988

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Author : Marie H. Tuttle
language : en
Publisher:
Release Date : 1988

Wind Tunnel Wall Interference January 1980 May 1988 written by Marie H. Tuttle and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1988 with Interference (Aerodynamics) categories.