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Multiple slot laminar film cooling.An analytical investigation is presented showing the effect of film cooling using single and double slots. The analysis considers the tangential injection of a gas of the same molecular weight as the main flow into a laminar boundary layer. Results in terms of heat transfer to the wall are presented for different slot heights, and injection velocities for both single and double slot configurations. The results indicate that the double slot is a more effective means of film cooling than the single slot.
Document ID
19720041562
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sherman, A.
(Computer and Applied Sciences, Inc. Norristown, Pa., United States)
Yeh, H.
(Pennsylvania, University Philadelphia, Pa., United States)
Reshotko, E.
(Case-Western-Reserve University Cleveland, Ohio, United States)
Mcassey, E., Jr.
(Villanova University Villanova, Pa., United States)
Date Acquired
August 6, 2013
Publication Date
April 1, 1972
Subject Category
Thermodynamics And Combustion
Report/Patent Number
AIAA PAPER 72-290
Report Number: AIAA PAPER 72-290
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Thermophysics Conference
Location: San Antonio, TX
Start Date: April 10, 1972
End Date: April 12, 1972
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
72A25228
Funding Number(s)
CONTRACT_GRANT: NASW-1866
Distribution Limits
Public
Copyright
Other

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