CAL/TRECOM Symposium Proceedings. Volume II. Dynamic Load Problems Associated with Helicopters and V/STOL Aircraft, June 26-28 Buffalo, N.Y.

摘要

Contents: A review of the structural dynamic characteristics of the XC-142A aircraft; propeller whirl flutter considerations for V/STOL aircraft; high-speed shafting for power transmission in aircraft; dynamic torsional problems in VTOL drive trains with universal joints; recent work at the Royal Aircraft Establishment on helicopter dynamic loads, with particular reference to high blade incidence problems; some results from the army low altitude, high-speed flight program (man-machine); human factor problems associated with low altitude high-speed (LAHS) flight; effect of gust alleviation system on dynamic airloads; and an analytical investigation of aircraft loads induced by rough terrain landings.