Accession Number:

ADA012094

Title:

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

Descriptive Note:

Corporate Author:

BELL AEROSPACE CO BUFFALO N Y

Report Date:

1969-12-01

Pagination or Media Count:

214.0

Abstract:

Tests of a 15 scale powered VSTOL 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.

Subject Categories:

  • Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE