Accession Number:

AD0767179

Title:

STOL Tactical Aircraft Investigation-Externally Blown Flap. Volume 1. Configuration Definition. Supplement 1. Aerodynamic Trades of Flap and Roll Control System

Descriptive Note:

Final rept. 10 Jun 1971-10 Dec 1972

Corporate Author:

ROCKWELL INTERNATIONAL LOS ANGELES CA LOS ANGELES AIRCRAFT DIV

Personal Author(s):

Report Date:

1973-04-01

Pagination or Media Count:

122.0

Abstract:

Contents Comparison of climb speeds Comparison of roll acceleration with all engines operating Comparison of roll acceleration with one engine inoperative Comparison of lift loss due to maximum roll control.

Subject Categories:

  • Aerodynamics
  • VSTOL

Distribution Statement:

APPROVED FOR PUBLIC RELEASE