TAKE-OFF DISTANCES OF A SUPERSONIC TRANSPORT CONFIGURATION AS AFFECTED BY AIRPLANE ROTATION DURING THE TAKE-OFF RUN

Abstract

An analytical study has been made to determine the effects of rotation speed, rotation angle, and rotation time on the take-off distance of a supersonic transport configuration. The takeoff distances were also determined at various rotation speeds to show the effects of such configuration changes as wing loading, maximum lift coefficient, thrust-weight ratio, and induced drag. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1961
Accession Number
AD0265481

Entities

People

  • Albert W. Hall

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airplanes
  • Coefficients
  • Fixed Wing Aircraft
  • Jet Aircraft
  • Rotation
  • Supersonic Aircraft
  • Supersonic Transport Aircraft
  • Transport Ships
  • Vehicles

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight