Edwards, J. W., & United States. National Aeronautics and Space Administration. (1996). Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method. [National Aeronautics and Space Administration].
Chicago Style (17th ed.) CitationEdwards, John W., and United States. National Aeronautics and Space Administration. Transonic Shock Oscillations and Wing Flutter Calculated with an Interactive Boundary Layer Coupling Method. [Washington, DC]: [National Aeronautics and Space Administration], 1996.
MLA (8th ed.) CitationEdwards, John W., and United States. National Aeronautics and Space Administration. Transonic Shock Oscillations and Wing Flutter Calculated with an Interactive Boundary Layer Coupling Method. [National Aeronautics and Space Administration], 1996.