Sonic line in nonequilibrium nozzle flows.

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Supersonic flow of reacting gases in de Laval nozzle for Mach number near unity

Document ID

19660059431

Acquisition Source

Legacy CDMS

Document Type

Reprint (Version printed in journal)

Authors

Date Acquired

August 3, 2013

Publication Date

August 1, 1966

Publication Information

Publication: AIAA JOURNAL

Subject Category

Accession Number

66A38721

Funding Number(s)

Distribution Limits

Public

Other

Keywords

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