APA (7th ed.) Citation

DeBonis, J. R., & Trefny, C. J. (2001). Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system. National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information.

Chicago Style (17th ed.) Citation

DeBonis, J. R., and C. J. Trefny. Supersonic Wind Tunnel Tests of a Half-axisymmetric 12⁰-spike Inlet to a Rocket-based Combined-cycle Propulsion System. [Cleveland, Ohio] : Hanover, MD: National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information, 2001.

MLA (9th ed.) Citation

DeBonis, J. R., and C. J. Trefny. Supersonic Wind Tunnel Tests of a Half-axisymmetric 12⁰-spike Inlet to a Rocket-based Combined-cycle Propulsion System. National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information, 2001.