Accession Number:

AD0819970

Title:

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

Descriptive Note:

Corporate Author:

ARMY TRANSPORTATION RESEARCH COMMAND FORT EUSTIS VA

Personal Author(s):

Report Date:

1963-06-28

Pagination or Media Count:

235.0

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.

Subject Categories:

  • Aerodynamics
  • Helicopters
  • VSTOL

Distribution Statement:

APPROVED FOR PUBLIC RELEASE