Maximum Lift Coefficients for Aerofoil Sections at Mach Numbers from 0.60 to 0.75 (Aerodynamics, v. W.01.01.07)

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  • ISBN10 1862464480
  • ISBN13 9781862464483
  • Publish Date December 1954
  • Publish Status Active
  • Publish Country GB
  • Publisher IHS ESDU
  • Imprint ESDU International PLC
  • Format Paperback
  • Pages 3
  • Language English