CAL/TRECOM SYMPOSIUM PROCEEDINGS VOL 1. DYNAMIC LOAD PROBLEMS ASSOCIATED WITH HELICOPTERS AND V/STOL AIRCRAFT, JUNE 26-28 1963, BUFFALO, NY

Abstract

Contents: Dynamic Loads in a Rigid Rotor from Full-Scale Wind-Tunnel Tests; An Aeroelastic Study of Helicopter Rotor Systems in High-Speed Flight; In-Flight Measurement of Steady and Oscillatory Rotor Shaft Loads; Full-Scale Flight Test Data Relating to Rotor Unsteady Aerodynamics; Experimental and Theoretical Study of Local Induced Velocities Over a Rotor Disc; Rotor Airloads; Comparison of Flight Measured Helicopter Rotor Blade Chordwise Pressure Distributions and Two-Dimensional Airfoil Characteristics; A Discussion of Rotor Blade Harmonic Airloading; and An Experimental Investigation of the Effect of a Non-Rigid Wake on Rotor Blade Airloads in Transition Flight.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jun 28, 1963
Accession Number
AD0819970

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Loading
  • Aircraft Equipment
  • Aircraft Industry
  • Aircrafts
  • Airframes
  • Artificial Intelligence
  • Dynamic Loads
  • Dynamic Response
  • Fluid Dynamics
  • Helicopter Rotors
  • Measurement
  • Pressure Distribution
  • Short Takeoff Aircraft
  • Strain Gages
  • Test Facilities
  • Three Dimensional
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Aerospace Engineering
  • Structural Dynamics.