An Evaluation of Nozzle Afterbody Code PDF Download

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An Evaluation of Nozzle Afterbody Code

An Evaluation of Nozzle Afterbody Code PDF Author: Frederick C. Guyton
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 68

Book Description

An Evaluation of Nozzle Afterbody Code

An Evaluation of Nozzle Afterbody Code PDF Author: Frederick C. Guyton
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 68

Book Description

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702

Book Description

Evaluation of Reynolds Number and Tunnel Wall Porosity Effects on Nozzle Afterbody Drag at Transonic Mach Numbers

Evaluation of Reynolds Number and Tunnel Wall Porosity Effects on Nozzle Afterbody Drag at Transonic Mach Numbers PDF Author: C. E. Robinson
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 38

Book Description
An experimental investigation was conducted to study the effects of Reynolds number variation on isolated nozzle afterbody performance. A strut-mounted cone-cylinder model with three separate afterbody configurations for Aerospace Research and Development (AGARD) was used for this investigation. This program was conducted in two phases distinguished by the model size and the wind tunnels used to obtain the experimental results. The effect of tunnel wall porosity on nozzle afterbody (NAB) performance was investigated.

Civil Engineering Hydraulics Abstracts

Civil Engineering Hydraulics Abstracts PDF Author:
Publisher:
ISBN:
Category : Hydraulic engineering
Languages : en
Pages : 518

Book Description

First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop

First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop PDF Author: Richard M. Wood
Publisher:
ISBN:
Category : High-speed aeronautics
Languages : en
Pages : 354

Book Description

Evaluation of Various Exhaust Nozzles at Free-stream Mach Numbers from 0.6 To. 3.0

Evaluation of Various Exhaust Nozzles at Free-stream Mach Numbers from 0.6 To. 3.0 PDF Author: Lawrence L. Galigher
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 128

Book Description

Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1636

Book Description

Flow Analysis and Design Optimization Methods for Nozzle Afterbody of a Hypersonic Vehicle

Flow Analysis and Design Optimization Methods for Nozzle Afterbody of a Hypersonic Vehicle PDF Author: Oktay Baysal
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 70

Book Description

A Nozzle Internal Performance Prediction Method

A Nozzle Internal Performance Prediction Method PDF Author: John R. Carlson
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 56

Book Description

Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages :

Book Description

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