Contents: Predicted and measured performance of two full-scale ducted propellers; Aerothermal dynamic performance of a high bypass tip turbine cruise fan system; Thrust deflection nozzles for VTOL aircraft; Shrouded propeller research at Mississippi State University leading to application on the United States Army XV-11A; The lift, drag and stability of wings immersed in propeller slipstream; Aerodynamic properties of airfoils in nonuniformly sheared flows; Experimental investigation of compound helicopter aerodynamic interference effects; Maximum lift coefficient for STOL aircraft: a critical review.
Cal/Usaavlabs Symposium Proceedings. Aerodynamic Problems Associated with V/STOL Aircraft. Volume II. Propulsion and Interference Aerodynamics. Held June 23, 1966, Statler-Hilton Hotel, Buffalo, New York
1966
330 pages
Report
Keine Angabe
Englisch