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A method for predicting the performance of high reaction supersonic compressor blade sections.Supersonic compressor blade sections performance prediction near maximum pressure ratio and efficiency by analyzing flow processes
Document ID
19690054722
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Boxer, E.
Date Acquired
August 5, 2013
Publication Date
June 1, 1969
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 69-522
Report Number: AIAA PAPER 69-522
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
69A32711
Distribution Limits
Public
Copyright
Other

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