Effects of nozzle exit location and shape on propulsion-induced aerodynamic characteristics due to vectoring twin nozzles at Mach numbers from 0.4 ̥to 1.2 /

Chicago citation style
Capone, Francis J. Effects of nozzle exit location and shape on propulsion-induced aerodynamic characteristics due to vectoring twin nozzles at Mach numbers from 0.4 ̥to 1.2 /. 1976. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011427313. (Accessed December 19, 2018.)
APA citation style
Capone, Francis J, (1976) Effects of nozzle exit location and shape on propulsion-induced aerodynamic characteristics due to vectoring twin nozzles at Mach numbers from 0.4 ̥to 1.2 /. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011427313
MLA citation style
Capone, Francis J. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011427313>.
Note: These citations are programmatically generated and may be incomplete.