Some observations on reduction of turbulent boundary-layer heat transfer in nozzles.

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Convective heat transfer in accelerated heated air flows through cooled conical supersonic nozzles of three different configurations

Document ID

19670036108

Acquisition Source

Legacy CDMS

Document Type

Reprint (Version printed in journal)

Authors

Date Acquired

August 3, 2013

Publication Date

December 1, 1966

Publication Information

Publication: AIAA JOURNAL

Subject Category

Accession Number

67A14837

Distribution Limits

Public

Other

Keywords

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