Slender-body Theory Based on Approximate Solution of the Transonic Flow Equation

Slender-body Theory Based on Approximate Solution of the Transonic Flow Equation
Author :
Publisher :
Total Pages : 252
Release :
ISBN-10 : NASA:31769000420011
ISBN-13 :
Rating : 4/5 ( Downloads)

Book Synopsis Slender-body Theory Based on Approximate Solution of the Transonic Flow Equation by : John R. Spreiter

Download or read book Slender-body Theory Based on Approximate Solution of the Transonic Flow Equation written by John R. Spreiter and published by . This book was released on 1959 with total page 252 pages. Available in PDF, EPUB and Kindle. Book excerpt: Approximate solutions of the nonlinear equations of the small disturbance theory of transonic flow are found for the pressure distribution on pointed slender bodies of revolution for flows with free-stream Mach number 1, and for flows that are either purely subsonic or purely supersonic. These results are obtained by application of a method based on local linearization that was introduced recently in the analysis of similar problems in low-dimensional flows. The theory is developed for bodies of arbitrary shapes, and specific results are given for cone-cylinders and for parabolic-arc bodies at zero angle of attack. All results are compared either with existing theoretical results or with experimental data.


Slender-body Theory Based on Approximate Solution of the Transonic Flow Equation Related Books

Slender-body Theory Based on Approximate Solution of the Transonic Flow Equation
Language: en
Pages: 252
Authors: John R. Spreiter
Categories: Aerodynamics
Type: BOOK - Published: 1959 - Publisher:

DOWNLOAD EBOOK

Approximate solutions of the nonlinear equations of the small disturbance theory of transonic flow are found for the pressure distribution on pointed slender bo
Slender-body Theory Based on Approximate Solution of Transonic Flow Equation [with List of References]
Language: en
Pages: 54
Slender-body Theory Based on Approximate Solution of the Transonic Flow Equation
Language: en
Pages: 60
Authors: John R. Spreiter
Categories: Aerodynamics
Type: BOOK - Published: 1959 - Publisher:

DOWNLOAD EBOOK

Summary: Approximate solutions of the nonlinear equations of the small disturbance theory of transonic flow are found for the pressure distribution on pointed s
Splender-body Theory Based on Approximate Solution of the Transonic Flow Equation
Language: en
Pages: 54
Authors: John R.. Spreiter
Categories:
Type: BOOK - Published: 1959 - Publisher:

DOWNLOAD EBOOK

NASA Technical Report
Language: en
Pages: 60
Authors:
Categories: Aerodynamics
Type: BOOK - Published: 1961 - Publisher:

DOWNLOAD EBOOK