Item Details

Performance of a Mach Number 3.0 Design Axisymmetric Double-Cone External-Compression Inlet in the Mach Number Range 1.97 to 0.79

by Owen H. Davis and Glenn A Mitchell
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration, 1960.
Language
English
Series
NASA Technical Memorandum
Description
29 p. : ill., graphs ; 27 cm.
Mode of access: Internet.
Notes
  • "Lewis Research Center, Cleveland, Ohio."
  • "N 63-16136."
  • "April 1960"--Cover.
  • Includes bibliographical references (p. 10).
Series Statement
NASA technical memorandum ; X-154
Logo for Copyright Not EvaluatedCopyright Not Evaluated
Technical Details

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    a| Performance of a Mach Number 3.0 design axisymmetric double-cone external-compression inlet in the mach number range 1.97 to 0.79 / c| by Owen H. Davis and Glenn A Mitchell.
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    a| Washington, D.C. : b| National Aeronautics and Space Administration, c| 1960.
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    a| 29 p. : b| ill., graphs ; c| 27 cm.
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    a| "April 1960"--Cover.
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    a| Includes bibliographical references (p. 10).
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    a| Mode of access: Internet.
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    a| Supersonic wind tunnels. 2| nasat
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    a| Inlet flow. 2| nasat
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    a| Graphs (charts). 2| nasat
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    a| Supersonic inlets. 2| nasat
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    a| Performance tests. 2| nasat
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    a| Mach number. 2| nasat
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    7
    a| Air intakes. 2| nasat
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    a| Aerodynamics, Supersonic.
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    a| Drag (Aerodynamics)
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    a| Jet engines x| Air intakes.
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    a| Mitchell, Glenn A.
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    a| Lewis Research Center.
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