Evaluation of a technique for determining airplane aileron effectiveness and roll rate by using an aeroelastically scaled model
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- Created Date
- 1969
- Description
Includes bibliographical references (p. 14).
Wind tunnel studies of scaled model of multijet cargo airplane.
- Creator
Abel, Irving
- Partner
- HathiTrust
- Contributing Institution
- University of Illinois
- Publisher
- Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151]
- Type
- text
- Format
- Language materialElectronic resource
- Language
- English
- Rights
- Public domain. Learn more at http://www.hathitrust.org/access_use
- Chicago citation style
- Abel, Irving. Evaluation of a technique for determining airplane aileron effectiveness and roll rate by using an aeroelastically scaled model. 1969. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011444738. (Accessed March 29, 2024.)
- APA citation style
- Abel, Irving, (1969) Evaluation of a technique for determining airplane aileron effectiveness and roll rate by using an aeroelastically scaled model. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011444738
- MLA citation style
- Abel, Irving. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011444738>.