Batina, J. T., & United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch. (1985). Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads. National Aeronautics and Space Administration, Scientific and Technical Information Branch.
Chicago Style (17th ed.) CitationBatina, John T., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch. Effects of Airfoil Shape, Thickness, Camber, and Angle of Attack on Calculated Transonic Unsteady Airloads. Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
MLA (8th ed.) CitationBatina, John T., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch. Effects of Airfoil Shape, Thickness, Camber, and Angle of Attack on Calculated Transonic Unsteady Airloads. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.