Subsonic aerodynamic characteristics of a large-scale 1.075-pressure-ratio tip-turbine cruise-fan propulsion system at angle of attack

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Created Date
[1969]
Description

Includes bibliographical references (p. 11).

Wind tunnel tests of subsonic aerodynamic characteristics of large scale tip turbine cruise fan with 1.075 pressure ratio at angle of attack.

Creator

Capone, Francis J

Partner
HathiTrust
Contributing Institution
University of Illinois
Publisher
Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230]
Subjects
Angle of attack (Aerodynamics)
Lift fans--Testing
Type
text
Format
Language material
Electronic resource
Language
English
URL
http://catalog.hathitrust.org/Record/011444686
Rights
Public domain. Learn more at http://www.hathitrust.org/access_use
Chicago citation style
Capone, Francis J. Subsonic aerodynamic characteristics of a large-scale 1.075-pressure-ratio tip-turbine cruise-fan propulsion system at angle of attack. [1969]. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011444686. (Accessed April 18, 2024.)
APA citation style
Capone, Francis J, ([1969]) Subsonic aerodynamic characteristics of a large-scale 1.075-pressure-ratio tip-turbine cruise-fan propulsion system at angle of attack. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011444686
MLA citation style
Capone, Francis J. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011444686>.
Note: These citations are programmatically generated and may be incomplete.