Design parameters for flow energizersOne of the most significant uses of flow energizers, which are small highly swept strakes mounted immediately above a lifting surface, is in flow control over regions where a lifting surface is joined to another body, such as a fuselage or nacelle. In the presently reported systematic wind tunnel test study of flow energizers, 14 different geometric configurations using a 75-deg sweep flow energizer were tested on a light twin-engine general aviation aircraft model. It is found that cambered flow energizers perform better than their flat counterparts. All but two of the energizer installations developed lower L/D at cruise angles of attack, lower maximum lift coefficients, and lower stall angles of attack than the baseline model.
Document ID
19850031419
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ward, D. T. (Texas A&M Univ. College Station, TX, United States)
Binford, R. S. (Texas A&M University College Station, TX, United States)
Date Acquired
August 12, 2013
Publication Date
October 1, 1984
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 84-2499Report Number: AIAA PAPER 84-2499