An investigation of several NACA 1-series inlets at Mach numbers from 0.4 to 1.29 for mass-flow ratios near 1.0

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Created Date
1976
Description

Cover title.

Includes bibliographical references (p. 12-13).

Creator

Re, Richard J

Partner
HathiTrust
Contributing Institution
University of Illinois
Publisher
Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service
Subjects
Airplanes--Turbojet engines--Air intakes
Aerofoils
Mach number
Type
text
Format
Language material
Electronic resource
Language
English
URL
http://catalog.hathitrust.org/Record/011427508
Rights
Public domain. Learn more at http://www.hathitrust.org/access_use
Chicago citation style
Re, Richard J. An investigation of several NACA 1-series inlets at Mach numbers from 0.4 to 1.29 for mass-flow ratios near 1.0. 1976. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011427508. (Accessed April 20, 2024.)
APA citation style
Re, Richard J, (1976) An investigation of several NACA 1-series inlets at Mach numbers from 0.4 to 1.29 for mass-flow ratios near 1.0. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011427508
MLA citation style
Re, Richard J. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011427508>.
Note: These citations are programmatically generated and may be incomplete.