Power Balance in Aerodynamic Flows
Author(s)
Drela, Mark
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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
2009-07Department
Massachusetts Institute of Technology. Department of Aeronautics and AstronauticsJournal
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