Aerodynamic characteristics of twin-propeller deflected-slipstream STOL airplane model with boundary-layer control on inverted V-tail
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- View Full Item
- Created Date
- 1968
- Description
Work performed at Langley Research Center.
N69-10935.
Includes bibliographical references (p. 16).
- Creator
Margason, Richard J
- Partner
- HathiTrust
- Contributing Institution
- University of Illinois
- Publisher
- Washington, D.C. : National Aeronautics and Space Administration
- Subjects
- Aerodynamics
Airplanes--Tail surfaces
Propellers, Aerial
Boundary layer control
Short take-off and landing aircraft - Type
- text
- Format
- Language materialElectronic resource
- Language
- English
- Rights
- Public domain. Learn more at http://www.hathitrust.org/access_use
- Chicago citation style
- Margason, Richard J. Aerodynamic characteristics of twin-propeller deflected-slipstream STOL airplane model with boundary-layer control on inverted V-tail. 1968. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011444586. (Accessed April 18, 2024.)
- APA citation style
- Margason, Richard J, (1968) Aerodynamic characteristics of twin-propeller deflected-slipstream STOL airplane model with boundary-layer control on inverted V-tail. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011444586
- MLA citation style
- Margason, Richard J. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011444586>.