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Power Balance in Aerodynamic Flows

Author(s)
Drela, Mark
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Article is made available in accordance with the publisher's policy and may be subject to US copyright law. Please refer to the publisher's site for terms of use.
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Abstract
A control volume analysis of the compressible viscous flow about an aircraft is performed,including integrated propulsors and flow control systems. In contrast to most past analyses which have focused on forces and momentum flow, in particular thrust and drag, the present analysis focuses on mechanical power and kinetic energy flow. The result is a clear identification and quantification of all the power sources, power sinks, and their interactions which are present in any aerodynamic flow. The formulation does not require any separate definitions of thrust and drag, and hence it is especially useful for analysis and optimization of aerodynamic configurations which have tightly integrated propulsion and boundary layer control systems.
Date issued
2009-07
URI
http://hdl.handle.net/1721.1/108322
Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Journal
AIAA Journal
Publisher
American Institute of Aeronautics and Astronautics
Citation
Drela, Mark. “Power Balance in Aerodynamic Flows.” AIAA Journal 47, no. 7 (July 2009): 1761–1771. © American Institute of Aeronautics and Astronautics
Version: Author's final manuscript
ISSN
0001-1452
1533-385X

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