Effects of wing leading-edge deflection on low-speed aerodynamic characteristics of a low-aspect-ratio highly swept arrow-wing configuration

Image
View Full Item
Created Date
1979
Description

Includes bibliographical references.

Creator

Coe, Paul L

Partner
HathiTrust
Contributing Institution
University of Illinois
Publisher
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch
Subjects
Leading edges (Aerodynamics)
Airplanes--Wings, Swept-back--Testing
Type
text
Format
Language material
Electronic resource
Language
English
URL
http://catalog.hathitrust.org/Record/011427487
Rights
Public domain. Learn more at http://www.hathitrust.org/access_use
Chicago citation style
Coe, Paul L. Effects of wing leading-edge deflection on low-speed aerodynamic characteristics of a low-aspect-ratio highly swept arrow-wing configuration. 1979. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011427487. (Accessed April 18, 2024.)
APA citation style
Coe, Paul L, (1979) Effects of wing leading-edge deflection on low-speed aerodynamic characteristics of a low-aspect-ratio highly swept arrow-wing configuration. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011427487
MLA citation style
Coe, Paul L. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011427487>.
Note: These citations are programmatically generated and may be incomplete.