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Leading edge cooling by upstream injectionA leading edge cooling system by upstream along the surface was investigated. The purpose of this system is to keep the leading edge below a desired temperature without excessively increasing the radius of the tip and consequently the total pressure losses. An experimental investigation was conducted to find the optimum conditions for the cooling from the point of view of upstream jet penetration and minimum shock losses. A theoretical analysis was performed to study the flow field in the mixing region between the two counterflowing streams and the results obtained compare favorably with the experimental results.
Document ID
19720005291
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Piva, R.
(New York Univ. New York, NY, United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-111965
Report Number: NASA-CR-111965
Accession Number
72N12940
Funding Number(s)
CONTRACT_GRANT: NGR-33-016-131
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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