PRELIMINARY FLIGHT TEST DATA UH-1B HIGH PERFORMANCE HELICOPTER

Abstract

This report presents the results of flight investigations conducted in association with the primary flight test investigation of the high performance UH-1 helicopter. Results reported include main rotor blades with inboard trailing edge flaps, a two-bladed flex beam rotor, and tapered tip main rotor blades.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1964
Accession Number
AD0627133

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Airframes
  • Airspeed
  • Aluminum Alloys
  • Assembly
  • Bending Moments
  • Blade Tips
  • Flight
  • Flight Speeds
  • Helicopters
  • Level Flight
  • Mach Number
  • Pilot Seats
  • Production
  • Secondary Flow
  • Spars
  • Trailing Edges
  • Vehicles

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Aerospace Engineering