A Method for Calculating the Aerodynamic Loading on Wing-body Combinations at Small Angles of Attack in Supersonic Flow

A Method for Calculating the Aerodynamic Loading on Wing-body Combinations at Small Angles of Attack in Supersonic Flow
Author :
Publisher :
Total Pages : 44
Release :
ISBN-10 : UIUC:30112106639849
ISBN-13 :
Rating : 4/5 ( Downloads)

Book Synopsis A Method for Calculating the Aerodynamic Loading on Wing-body Combinations at Small Angles of Attack in Supersonic Flow by : Charlie M. Jackson

Download or read book A Method for Calculating the Aerodynamic Loading on Wing-body Combinations at Small Angles of Attack in Supersonic Flow written by Charlie M. Jackson and published by . This book was released on 1971 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes a theoretical method for estimating the aerodynamic loading on a wing-body configuration. In order to provide a basis for evaluation of the method, experimental measurements of surface pressures, forces, and moments were made on a series of basic wing-body configurations over a Mach number range from 2.5 to 4.5. Comparison of the theoretical estimates with these experimental data generally indicated good agreement for the entire range of configurations and test conditions.


A Method for Calculating the Aerodynamic Loading on Wing-body Combinations at Small Angles of Attack in Supersonic Flow Related Books

A Method for Calculating the Aerodynamic Loading on Wing-body Combinations at Small Angles of Attack in Supersonic Flow
Language: en
Pages: 44
Authors: Charlie M. Jackson
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1971 - Publisher:

DOWNLOAD EBOOK

This report describes a theoretical method for estimating the aerodynamic loading on a wing-body configuration. In order to provide a basis for evaluation of th
A Method for Calculating the Aerodynamic Loading on Wing-body Combinations at Small Angles of Attack in Supersonic Flow
Language: en
Pages: 0
Authors: Charlie M. Jackson
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1971 - Publisher:

DOWNLOAD EBOOK

A Method for Calculating the Aerodynamic Loading on Wing-body Combinations at Small Angles of Attck in Supersonic Flow
Language: en
Pages: 32
A Method for Calculating Aerodynamic Loadings on Thin Wings at a Mach Number of 1
Language: en
Pages: 38
Authors: John L. Crigler
Categories: Aerodynamic load
Type: BOOK - Published: 1959 - Publisher:

DOWNLOAD EBOOK

NASA Technical Note
Language: en
Pages: 508
Authors:
Categories:
Type: BOOK - Published: 1971 - Publisher:

DOWNLOAD EBOOK