Aerodynamic characteristics of a series of twin-inlet air-breathing missile configurations

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Created Date
1983
Description

"March 1983"--Cover.

Includes bibliographical references.

1. Axisymmetric inlets at supersonic speeds -- 2. Two-dimensional inlets at supersonic speeds -- 3. Axisymmetric and two-dimensional inlets at subsonic-transonic speeds.

Creator

Hayes, Clyde

Partner
HathiTrust
Contributing Institution
University of Illinois
Publisher
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service]
Subjects
Aerodynamics
Stability
Guided missiles--Control systems
Type
text
Format
Language material
Electronic resource
Language
English
URL
http://catalog.hathitrust.org/Record/011427126
Rights
Public domain. Learn more at http://www.hathitrust.org/access_use
Chicago citation style
Hayes, Clyde. Aerodynamic characteristics of a series of twin-inlet air-breathing missile configurations. 1983. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011427126. (Accessed April 19, 2024.)
APA citation style
Hayes, Clyde, (1983) Aerodynamic characteristics of a series of twin-inlet air-breathing missile configurations. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011427126
MLA citation style
Hayes, Clyde. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011427126>.
Note: These citations are programmatically generated and may be incomplete.