The ability of current methodologies to accurately predict the aerodynamic characteristics identified as uncertainties was evaluated for two aircraft configurations. The two wind tunnel models studied horizontal altitude takeoff and landing V/STOL fighter aircraft derivatives.
Analysis of Wind Tunnel Test Results for a 9.39-Per Cent Scale Model of a Vstol Fighter/Attack Aircraft. Volume 1: Study Overview
1980
97 pages
Report
Keine Angabe
Englisch