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Prandtl-Meyer angle in supersonic nozzle

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Old   November 7, 2000, 02:22
Default Prandtl-Meyer angle in supersonic nozzle
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98.4F
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What is the signifance of the Prandtl-Meyer angle in flow problems and why is it so important in supersonic nozzle flow?

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Old   November 8, 2000, 05:20
Default HEY IS ANYONE OUT THERE I REALLY NEED INFO ON THIS
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98.4F
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Especially if anyone knows of a reference to calculate nozzle contours for a variable mach number 2D supersonic nozzle with subsonic portion, portion from throat to inflection point, partial cancellation region and full calcellation region.

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Old   November 8, 2000, 12:27
Default Re: HEY IS ANYONE OUT THERE I REALLY NEED INFO ON
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John C. Chien
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(1). Most gas dynamics text books should have chapters related to MOC (method of characteristics) applications. (2). Type "nozzle moc analysis" into a websearch site, and you should be able to find more recent information. (3). Check into the NASA websites, such as Langley, or Lewis (now Glenn). They should have all the information related to the supersonic nozzle design.
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Old   December 4, 2009, 17:05
Default code???
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staleyjj1981 is on a distinguished road
I need a code for designing a diverging section of a 2-D minimum length shock free nozzle using methods of characteristics preferably matlab....any one know where to get it????
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