Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 ̊clipped-delta-wing orbiter configuration at supersonic mach numbers /
A.B. Blair, Jr. ; Langley Research Center, Hampton, Va.

APA Citation

Blair, A. B., United States. National Aeronautics and Space Administration., Langley Research Center. (1976). Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 ̊clipped-delta-wing orbiter configuration at supersonic mach numbers. Washington: U.S. National Aeronautics and Space Administration .

MLA Citation

Blair, A. B, United States. National Aeronautics and Space Administration, and Langley Research Center. Effect of Reynolds Number On the Aerodynamic Stability And Control Characteristics of a 55 ̊clipped-delta-wing Orbiter Configuration At Supersonic Mach Numbers. Washington: U.S. National Aeronautics and Space Administration , 1976.