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Heat transfer and thermal boundary layer in a conical nozzle.Inlet thermal boundary layer thickness effect on conical nozzle heat transfer and boundary layer determined by operating nozzle with cooled/ uncooled inlet
Document ID
19690054791
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Boldman, D. R.
Graham, R. W.
Date Acquired
August 5, 2013
Publication Date
June 1, 1969
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Thermodynamics And Combustion
Report/Patent Number
AIAA PAPER 69-474
Report Number: AIAA PAPER 69-474
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE
Location: COLORADO SPRINGS, COLO.
Start Date: June 9, 1969
End Date: June 13, 1969
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
69A32780
Distribution Limits
Public
Copyright
Other

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