IN-FLIGHT MEASUREMENT AND CORRELATION WITH THEORY OF BLADE AIRLOADS AND RESPONSES ON THE XH-51A COMPOUND HELICOPTER ROTOR. VOLUME 2. MEASUREMENT AND DATA REDUCTION OF AIRLOADS AND STRUCTURAL LOADS. APPENDIXES 5 THROUGH 9

Abstract

Contents: Differential pressure -- dynamic components; Differential pressure -- static components; Blade loads -- dynamic and static components; Harmonic components of airloads and pitching moments; Harmonic components of structural loads.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
May 01, 1968
Accession Number
AD0674194

Entities

People

  • E. A. Bartsch

Organizations

  • Lockheed Martin

Tags

Communities of Interest

  • C4I
  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Army Aviation
  • California
  • Computer Programs
  • Contracts
  • Data Processing
  • Data Reduction
  • Harmonic Analysis
  • Helicopter Rotors
  • Helicopters
  • Measurement
  • Plastic Explosives
  • Pressure Measurement
  • Structural Loads
  • Tank Guns
  • Two Dimensional
  • United States

Readers

  • Aerodynamics.
  • Structural Dynamics.