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

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.

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Document Details

Document Type
Technical Report
Publication Date
Jun 22, 1966
Accession Number
AD0657562

Entities

Organizations

  • Calspan

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aircrafts
  • Boundary Layer
  • Computational Fluid Dynamics
  • Computational Science
  • Flow Visualization
  • Fluid Dynamics
  • Hydrodynamics
  • Measurement
  • Mechanical Properties
  • Pressure Gages
  • Pressure Measurement
  • Pressure Transducers
  • Short Takeoff Aircraft
  • Strain Gages
  • Three Dimensional
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Academic Conference Management
  • Aerospace Engineering
  • Fluid Mechanics and Fluid Dynamics.