Measured and Theoretical Flow Fields Behind a Rectangular and a Triangular Wing Up to High Angles of Attack at a Mach Number of 2.46

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  • Measured and Theoretical Flow Fields Behind a Rectangular and a Triangular Wing Up to High Angles of Attack at a Mach Number of 2.46 Book Detail

  • Author : Frank J. Centolanzi
  • Release Date : 1959
  • Publisher :
  • Genre : Mach number
  • Pages : 82
  • ISBN 13 :
  • File Size : 19,19 MB

Measured and Theoretical Flow Fields Behind a Rectangular and a Triangular Wing Up to High Angles of Attack at a Mach Number of 2.46 by Frank J. Centolanzi PDF Summary

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