Flight Measurements of the Lateral Response Characteristics of the Convair XF-92A Delta-Wing Airplane
Description:
Memorandum presenting rudder pulse maneuvers obtained with the Convair XF-92A delta-wing research airplane at an altitude of about 30,000 feet over a Mach number range of 0.52 to 0.92. Tests were made with and without a wing fence. By analyzing the maneuvers, the characteristics of the airplane transient, airplane stability derivatives, and frequency-response characteristics were measured.
Date:
August 5, 1955
Creator:
Holleman, Euclid C.
Partner:
UNT Libraries Government Documents Department