Powell, A. G., Agrawal, S., Lacey, T. R., & Langley Research Center. (1989). Feasibility and benefits of laminar flow control on supersonic cruise airplanes. National Aeronautics and Space Administration, Langley Research Center.
Chicago Style (17th ed.) CitationPowell, A. G., Sudhir Agrawal, T. R. Lacey, and Langley Research Center. Feasibility and Benefits of Laminar Flow Control on Supersonic Cruise Airplanes. Hampton, Va.: National Aeronautics and Space Administration, Langley Research Center, 1989.
MLA (8th ed.) CitationPowell, A. G., et al. Feasibility and Benefits of Laminar Flow Control on Supersonic Cruise Airplanes. National Aeronautics and Space Administration, Langley Research Center, 1989.
Warning: These citations may not always be 100% accurate.