Theoretical and experimental study of twisted and cambered delta wings designed for a mach number of 3.5 /

Chicago citation style
Sorrells, Russell B. Theoretical and experimental study of twisted and cambered delta wings designed for a mach number of 3.5 /. 1976. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011444003. (Accessed November 17, 2018.)
APA citation style
Sorrells, Russell B, (1976) Theoretical and experimental study of twisted and cambered delta wings designed for a mach number of 3.5 /. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011444003
MLA citation style
Sorrells, Russell B. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011444003>.
Note: These citations are programmatically generated and may be incomplete.