Exploratory low-speed wind-tunnel investigation of advanced commuter configurations including an over-the-wing propeller designA recent low-speed wind-tunnel investigation of a three-surface regional transport configuration has shown large favorable power effects on longitudinal and lateral stability and marginal engine-out trim characteristics for some aft engine and empennage configurations. The present paper discusses these results in terms of static force test information obtained for power-off and power-on conditions. Also discussed in this paper are wind-tunnel results which indicate that mounting propellers over the wing can introduce large favorable slipstream interference effects which significantly reduce the wing drag at climb power conditions.
Document ID
19830068372
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Johnson, J. L., Jr. (NASA Langley Research Center Hampton, VA, United States)
White, E. R. (Kentron International, Inc., Technical Center Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
October 1, 1983
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 83-2531Report Number: AIAA PAPER 83-2531