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

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.

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Document Details

Document Type
Technical Report
Publication Date
Jun 24, 1966
Accession Number
AD0657564

Entities

Organizations

  • Calspan

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aircraft Equipment
  • Aircraft Industry
  • Aircrafts
  • Airframes
  • Boundary Layer
  • Boundary Layer Flow
  • Computational Fluid Dynamics
  • Flow Fields
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Mechanics
  • Helicopter Rotors
  • Pressure Distribution
  • Rotary Wing Aircraft
  • Secondary Flow
  • Short Takeoff Aircraft

Fields of Study

  • Physics

Readers

  • Academic Conference Management
  • Aerodynamics.
  • Aerospace Engineering