Accession Number : ADA012094

Title :   Wind Tunnel Test Data Report of a Powered 1/5 Scale ARL/Bell V/STOL Aircraft Model. Phase II,

Corporate Author : BELL AEROSPACE CO BUFFALO N Y

Personal Author(s) : Ryan,P. E. ; Henderson,C. ; Breidenstein,R. M. ; Hesby,A. T.

Report Date : DEC 1969

Pagination or Media Count : 214

Abstract : Tests of a 1/5 scale powered V/STOL aircraft model were conducted in the Langley 7 x 10 wind tunnel. Vehicle aerodynamics and stability and control characteristics were investigated. The test results are presented without analysis.

Descriptors :   *Vertical takeoff aircraft, *Wind tunnel tests, *Model tests, Aerodynamic characteristics, Stability, Control, Subsonic characteristics, Test facilities, Flaps(Control surfaces), Test methods, Short takeoff aircraft, Thrust augmentation, Hovering, Level flight, Booms(Equipment), Transitions, Angle of attack, Sideslip, Control surfaces, Ejectors

Subject Categories : Aerodynamics

Distribution Statement : APPROVED FOR PUBLIC RELEASE