Search Results - "Y 3.N 21/5:6/2711"
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The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section /
Published 1952“…Y 3.N 21/5:6/2711…”
Government Document Book -
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The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section /
Published 1952“…Y 3.N 21/5:6/2711…”
Online Access
Government Document eBook