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book (13)


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Book
Achievement of continuous wall curvature in design of two-dimensional symmetrical supersonic nozzles
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Year: 1952 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,

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Exploratory investigation of flow field resulting from forward-facing nozzles exhausting near a large cylindrical body at free-stream Mach numbers of 3.0 and 6.0
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Year: 1969 Publisher: Washington, D.C. : National Aeronautics and Space Administration,

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Book
Achievement of continuous wall curvature in design of two-dimensional symmetrical supersonic nozzles
Authors: --- ---
Year: 1952 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,

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Book
Exploratory investigation of flow field resulting from forward-facing nozzles exhausting near a large cylindrical body at free-stream Mach numbers of 3.0 and 6.0
Authors: --- --- ---
Year: 1969 Publisher: Washington, D.C. : National Aeronautics and Space Administration,

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The aerodynamic design and calibration of an asymmetric variable Mach number nozzle with a sliding block for the Mach number range 1.27 to 2.75
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Year: 1953 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,

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An accurate and rapid method for the design of supersonic nozzles
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Year: 1955 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,

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Book
The aerodynamic design and calibration of an asymmetric variable Mach number nozzle with a sliding block for the Mach number range 1.27 to 2.75
Authors: --- ---
Year: 1953 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,

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Book
An accurate and rapid method for the design of supersonic nozzles
Authors: --- ---
Year: 1955 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,


Book
The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section
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Year: 1952 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,

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An automated DAKOTA and VULCAN-CFD framework with application to supersonic facility nozzle flowpath optimization
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Year: 2015 Publisher: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center,

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