Investigation of the Aerodynamic Characteristics of a Hypersonic Transport Model at Mach Numbers to 6

Investigation of the Aerodynamic Characteristics of a Hypersonic Transport Model at Mach Numbers to 6
Author :
Publisher :
Total Pages : 92
Release :
ISBN-10 : UIUC:30112106691956
ISBN-13 :
Rating : 4/5 (56 Downloads)

Book Synopsis Investigation of the Aerodynamic Characteristics of a Hypersonic Transport Model at Mach Numbers to 6 by : James C. Ellison

Download or read book Investigation of the Aerodynamic Characteristics of a Hypersonic Transport Model at Mach Numbers to 6 written by James C. Ellison and published by . This book was released on 1971 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: Also available online.


Investigation of the Aerodynamic Characteristics of a Hypersonic Transport Model at Mach Numbers to 6 Related Books

Investigation of the Aerodynamic Characteristics of a Hypersonic Transport Model at Mach Numbers to 6
Language: en
Pages: 92
Authors: James C. Ellison
Categories: Aerodynamics, Hypersonic
Type: BOOK - Published: 1971 - Publisher:

DOWNLOAD EBOOK

Also available online.
Aerodynamic Characteristics of a Hypersonic Transport Configuration at Mach 6.86
Language: en
Pages: 36
Authors: William John Small
Categories: Aerodynamics
Type: BOOK - Published: 1970 - Publisher:

DOWNLOAD EBOOK

Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing
Language: en
Pages: 84
An Experimental Investigation of the Aerodynamic Characteristics of Slender Hypersonic Vehicles at High Angles of Attack
Language: en
Pages: 148
Authors: Robert H. Feldhuhn
Categories: Angle of attack (Aerodynamics)
Type: BOOK - Published: 1968 - Publisher:

DOWNLOAD EBOOK

Pressure, heat transfer, force, flow field surveys and flow visualization measurements on an inclined cone were obtained in a wind tunnel at a nominal Mach numb
Investigation of the Aerodynamic Characteristics of a Supersonic Horizontal- Attitude VTOL Airplane Model at Mach Numbers of 1.57, 2.14, 2.54, and 2.87
Language: en
Pages: 164