Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads
- Image
- View Full Item
- Created Date
- 1985
- Description
Prepared at Langley Research Center.
"March 1985"--Cover.
Includes bibliographical references (p. 10).
- Creator
Batina, John T
- 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
- Aerodynamic load
Aerodynamics, Transonic
Unsteady flow (Aerodynamics)
Camber (Aerofoils)
Aerofoils - Type
- text
- Format
- Language materialElectronic resource
- Language
- English
- Rights
- Public domain. Learn more at http://www.hathitrust.org/access_use
- Chicago citation style
- Batina, John T. Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads. 1985. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011427160. (Accessed April 19, 2024.)
- APA citation style
- Batina, John T, (1985) Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011427160
- MLA citation style
- Batina, John T. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011427160>.