Tweedt, D. L. (2014). Computational aerodynamic simulations of an 840 ft/sec tip speed advanced ducted propulsor fan system model for acoustic methods assessment and development. National Aeronautics and Space Administration, Glenn Research Center.
Chicago Style (17th ed.) CitationTweedt, Daniel L. Computational Aerodynamic Simulations of an 840 Ft/sec Tip Speed Advanced Ducted Propulsor Fan System Model for Acoustic Methods Assessment and Development. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2014.
MLA (9th ed.) CitationTweedt, Daniel L. Computational Aerodynamic Simulations of an 840 Ft/sec Tip Speed Advanced Ducted Propulsor Fan System Model for Acoustic Methods Assessment and Development. National Aeronautics and Space Administration, Glenn Research Center, 2014.