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Unsteady airfoil stall review and extensionUnsteady airfoil stall in incompressible flow, including pitch rate induced accelerated flow effect on leading edge and trailing edge stall
Document ID
19700042121
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ericsson, L. E.
Reding, J. P.
Date Acquired
August 5, 2013
Publication Date
January 1, 1970
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 70-77
Report Number: AIAA PAPER 70-77
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AEROSPACE SCIENCES MEETING, 8TH
Location: NEW YORK, NY
Start Date: January 19, 1970
End Date: January 21, 1970
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
70A18237
Funding Number(s)
CONTRACT_GRANT: NAS1-7999
Distribution Limits
Public
Copyright
Other

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