A Wind Tunnel Investigation At A Mach Number Of 201 Of The Sonic Boom Characteristics Of Three Wing Body Combinations Differing In Wing Longitudinal Location PDF Download

Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download A Wind Tunnel Investigation At A Mach Number Of 201 Of The Sonic Boom Characteristics Of Three Wing Body Combinations Differing In Wing Longitudinal Location PDF full book. Access full book title A Wind Tunnel Investigation At A Mach Number Of 201 Of The Sonic Boom Characteristics Of Three Wing Body Combinations Differing In Wing Longitudinal Location.

Wind-tunnel Investigation of the Static Longitudinal and Lateral Stability of a 1/62-scale Model of the X-1E at Supersonic Speeds

Wind-tunnel Investigation of the Static Longitudinal and Lateral Stability of a 1/62-scale Model of the X-1E at Supersonic Speeds
Author: Arthur Henderson
Publisher:
Total Pages: 94
Release: 1956
Genre: Aerodynamics, Supersonic
ISBN:

Download Wind-tunnel Investigation of the Static Longitudinal and Lateral Stability of a 1/62-scale Model of the X-1E at Supersonic Speeds Book in PDF, ePub and Kindle

An investigation to determine the static longitudinal and lateral stability characteristics of a 1/62-scale model of the X-1E has been conducted in the Langley 9-inch supersonic tunnel. Tests were made at Mach numbers of 1.62, 1.94, 2.22, 2.40, and 2.62 on the wing-body, wing-body-vertical-tail, and complete model configurations. Detailed analysis of the test results has not been made.