Csank, J. T., & Stueber, T. J. (2013). Advanced shock position control for mode transition in a turbine based combined cycle engine inlet model. National Aeronautics and Space Administration, Glenn Research Center.
Chicago Style (17th ed.) CitationCsank, Jeffrey T., and Thomas J. Stueber. Advanced Shock Position Control for Mode Transition in a Turbine Based Combined Cycle Engine Inlet Model. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2013.
MLA (9th ed.) CitationCsank, Jeffrey T., and Thomas J. Stueber. Advanced Shock Position Control for Mode Transition in a Turbine Based Combined Cycle Engine Inlet Model. National Aeronautics and Space Administration, Glenn Research Center, 2013.
Warning: These citations may not always be 100% accurate.