Capone, F. 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. U.S. National Aeronautics and Space Administration.
Chicago Style (17th ed.) CitationCapone, 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. Washington: U.S. National Aeronautics and Space Administration, 1976.
MLA (9th ed.) CitationCapone, 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. U.S. National Aeronautics and Space Administration, 1976.
Warning: These citations may not always be 100% accurate.