Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 ̊swept Double-delta Wing at Mach Numbers from 0.80 to 1.20, with Summary of Data from 0.20 to 6.0
Author : Jim A. Penland
Publisher :
Page : 150 pages
File Size : 23,17 MB
Release : 1979
Category : Aerodynamics
ISBN :