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Computational and Analytical Investigation of Aerodynamic Derivatives of Similitude Delta Wing Model at Hypersonic Speeds



  ID Publisher : 0000026254
  Nama Jurnal : International Journal of Technology
  Pengarang : Musayir Bashir, S.A. Khan, Qummare Azam, Ayub Ahmed Janvekar
  Subjek : Damping derivatives; Hypersonic flow; Piston theory; Stiffness derivatives; Wedge model
  Edisi : 8 / 3 / April 2017


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