Accession Number:

AD0720740

Title:

Stability and Controllability of Supersonic Aircraft,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1970-12-04

Pagination or Media Count:

9.0

Abstract:

A general description is given of methods by which a pilot can control the lateral motion of a supersonic aircraft.

Subject Categories:

  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE