Accession Number:

AD0657562

Title:

CAL/USAAVLABS SYMPOSIUM PROCEEDINGS. AERODYNAMIC PROBLEMS ASSOCIATED WITH V/STOL AIRCRAFT. VOLUME 1. PROPELLER AND ROTOR AERODYNAMICS. HELD JUNE 22, 1966, STATLER-HILTON HOTEL, BUFFALO, NEW YORK

Descriptive Note:

Corporate Author:

CORNELL AERONAUTICAL LAB INC BUFFALO NY

Personal Author(s):

Report Date:

1966-06-22

Pagination or Media Count:

279.0

Abstract:

Contents A theory for static propeller performance Propeller testing at zero velocity Propeller research at Canadair Limited Prediction of the performance and stress characteristics of VTOL propellers Performance potential of rotor blade inboard aerodynamic devices Aerodynamic loading of high-speed rotors Prediction of rotor wake flows The movement, structure and breakdown of trailing vortices from a rotor blade.

Subject Categories:

  • Aerodynamics
  • Helicopters
  • VSTOL
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE