Accession Number:

AD0657564

Title:

CAL/USAAVLABS SYMPOSIUM PROCEEDINGS. AERODYNAMIC PROBLEMS ASSOCIATED WITH V/STOL AIRCRAFT. VOLUME 3. AERODYNAMIC RESEARCH ON BOUNDARY LAYERS. HELD JUNE 24, 1966, STATLER-HILTON HOTEL, BUFFALO, NEW YORK

Descriptive Note:

Corporate Author:

CORNELL AERONAUTICAL LAB INC BUFFALO NY

Personal Author(s):

Report Date:

1966-06-24

Pagination or Media Count:

151.0

Abstract:

Contents Spanwise flow effects on rotor performance A preliminary study of the effect of a radial pressure gradient on the boundary layer of a rotor blade The boundary layer of the hovering rotor An investigation of the feasibility of a common boundary layer control system for high-lift and low-drag on an airfoil section.

Subject Categories:

  • Aerodynamics
  • Helicopters
  • VSTOL
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE