Browsing Aerospace Computational Design Laboratory: Technical Reports by Author "Lee, Kuok Ming"

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    • Numerical Simulation of Hypersonic Flow Over a Blunt Leading Edge Delta Wing 

      Lee, Kuok Ming (Aerospace Computational Design Lab, Dept. of Aeronautics & Astronautics, Massachusetts Institute of Technology, 1989-10)
      Euler and Navier-Stokes results are presented for a blunt delta wing at Mach 7.15 and 300 angle of attack. The viscous calculations were done at a Reynolds number based on chord of 5.85 x 106 with freestream and wall ...