Accession Number:

AD0657563

Title:

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

Descriptive Note:

Corporate Author:

CORNELL AERONAUTICAL LAB INC BUFFALO NY

Report Date:

1966-06-23

Pagination or Media Count:

331.0

Abstract:

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.

Subject Categories:

  • Aerodynamics
  • Helicopters
  • VSTOL
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE