Accession Number:

ADA019323

Title:

Recovery Techniques for Aircraft in Spinning Flight.

Descriptive Note:

Master's thesis,

Corporate Author:

AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH SCHOOL OF ENGINEERING

Personal Author(s):

Report Date:

1975-12-01

Pagination or Media Count:

130.0

Abstract:

This study represents an attempt to use numerical solutions of the equations of motion to discover the most effective control surface deflections for use in a delta-winged fighter for recovery from a fully developed spin. The recovery methods were tested upon stable spins since the stable flat spin is generally the most dangerous spin.

Subject Categories:

  • Aerodynamics
  • Attack and Fighter Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE