AN EVALUATION OF AN ANALYTICAL TECHNIQUE FOR THE PREDICTION OF THE SPIN AND SPIN RECOVERY CHARACTERISTICS OF A CONTEMPORARY AIRPLANE

Abstract

THE EVALUATION OF AN ANALYTICAL METHOD FOR THE PREDICTION OF SPIN AND SPIN RECOVERY CHARACTERISTICS OF A CONTEMPORARY AIRPLANE IS DESCRIBED. The spin characteristics of an airplane can be accurately determined through the use of static wind tunnel data and estimated rotary and damping derivations based on static wind tunnel data. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 15, 1961
Accession Number
AD0265789

Entities

People

  • R.h. Hanna

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airplanes
  • Fixed Wing Aircraft
  • Recovery
  • Spin Recovery
  • Test And Evaluation
  • Test Facilities
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Computational Modeling and Simulation