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Aerodynamics of heat exchangers for high-altitude aircraftReduction of convective beat transfer with altitude dictates unusually large beat exchangers for piston- engined high-altitude aircraft The relatively large aircraft drag fraction associated with cooling at high altitudes makes the efficient design of the entire heat exchanger installation an essential part of the aircraft's aerodynamic design. The parameters that directly influence cooling drag are developed in the context of high-altitude flight Candidate wing airfoils that incorporate heat exchangers are examined. Such integrated wing-airfoil/heat-exchanger installations appear to be attractive alternatives to isolated heat.exchanger installations. Examples are drawn from integrated installations on existing or planned high-altitude aircraft.
Document ID
19960033266
Acquisition Source
Ames Research Center
Document Type
Reprint (Version printed in journal)
Authors
Drela, Mark
(Massachusetts Inst. of Tech. Cambridge, MA United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1996
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-201078
AIAA Paper 95-1866
NAS 1.26:201078
Report Number: NASA-CR-201078
Report Number: AIAA Paper 95-1866
Report Number: NAS 1.26:201078
Meeting Information
Meeting: AIAA Applied Aerodynamics Conference
Location: San Diego, CA
Country: United States
Start Date: June 19, 1995
End Date: June 22, 1995
Sponsors: American Inst. of Aeronautics and Astronautics
Accession Number
96N30070
Funding Number(s)
CONTRACT_GRANT: NAG2-4008
Distribution Limits
Public
Copyright
Public Use Permitted.
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