Investigation at Mach Numbers 1.5 and 1.7 of Twin-duct Side Intake System with Two-dimensional 6 Degree Compression Ramps Mounted on a Supersonic Airplane

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  • Investigation at Mach Numbers 1.5 and 1.7 of Twin-duct Side Intake System with Two-dimensional 6 Degree Compression Ramps Mounted on a Supersonic Airplane Book Detail

  • Author : Joseph Davids
  • Release Date : 1953
  • Publisher :
  • Genre :
  • Pages : 29
  • ISBN 13 :
  • File Size : 57,57 MB

Investigation at Mach Numbers 1.5 and 1.7 of Twin-duct Side Intake System with Two-dimensional 6 Degree Compression Ramps Mounted on a Supersonic Airplane by Joseph Davids PDF Summary

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