Aerodynamic characteristics at Mach numbers of 1.5, 1.8, and 2.0 of a blended wing-body configuration with and without integral canards

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Created Date
1979
Description

May 1979.

Includes bibliographical references.

Creator

Robins, A. Warner

Partner
HathiTrust
Contributing Institution
University of Illinois
Publisher
[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Office
Subjects
Stability of airplanes
Hypersonic planes
Type
text
Format
Language material
Electronic resource
Language
English
URL
http://catalog.hathitrust.org/Record/011427373
Rights
Public domain. Learn more at http://www.hathitrust.org/access_use
Chicago citation style
Robins, A. Warner. Aerodynamic characteristics at Mach numbers of 1.5, 1.8, and 2.0 of a blended wing-body configuration with and without integral canards. 1979. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011427373. (Accessed April 20, 2024.)
APA citation style
Robins, A. Warner, (1979) Aerodynamic characteristics at Mach numbers of 1.5, 1.8, and 2.0 of a blended wing-body configuration with and without integral canards. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011427373
MLA citation style
Robins, A. Warner. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011427373>.
Note: These citations are programmatically generated and may be incomplete.