Application of shock tubes to transonic airfoil testing at high Reynolds numbers /

Chicago citation style
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office. Application of shock tubes to transonic airfoil testing at high Reynolds numbers /. 1978. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011427070. (Accessed December 15, 2018.)
APA citation style
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, (1978) Application of shock tubes to transonic airfoil testing at high Reynolds numbers /. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011427070
MLA citation style
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011427070>.
Note: These citations are programmatically generated and may be incomplete.