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“Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6” Metadata:

  • Title: ➤  Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6
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“Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6” Subjects and Themes:

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  • The Open Library ID: OL11306575W

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1Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6

“Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6” Metadata:

  • Title: ➤  Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch
  • Publish Date:
  • Publish Location: Washington, D.C

“Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6” Subjects and Themes:

Edition Identifiers:

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2Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6

“Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6” Metadata:

  • Title: ➤  Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch
  • Publish Date:
  • Publish Location: Washington, D.C

“Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6” Subjects and Themes:

Edition Identifiers:

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