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Experimental and numerical investigation of boundary-layer development and transition on the walls of a mach 5 nozzle

Experimental and numerical investigation of boundary-layer development and transition on the walls of a mach 5 nozzle - - Washington, D.C. NASA 1975 - 86 p. - NASA TN D-7976 : 1975 .

ISBN:

Subjects--Topical Terms:

Boundary-layer stability & transition, Nozzle and channel flow, Supersonic and hypersonic flow

Universal Decimal Class. No.: LNASA TN D-7976 : 1975

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