Supersonic, four shock, ramp type intake design, with internal boundary layer bleed

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dc.contributor.authorVan Staden, Paul Arnold
dc.contributor.otherStellenbosch University. Faculty of . Dept. of .
dc.date.accessioned2012-08-27T12:26:52Z
dc.date.available2012-08-27T12:26:52Z
dc.date.issued1990
dc.descriptionThesis (M. Eng. (Aeronautics)) -- University of Stellenbosch, 1990.
dc.descriptionFull text to be digitised and attached to bibliographic record.
dc.format.extent107 p. : ill.
dc.identifier.urihttp://hdl.handle.net/10019.1/68986
dc.language.isoen_ZA
dc.publisherStellenbosch : Stellenbosch University
dc.rights.holderStellenbosch University
dc.subjectGas-turbines -- Aerodynamics
dc.subjectAircraft gas-turbines -- Design and construction
dc.subjectAirplanes -- Ramjet engines -- Air intakes
dc.subjectDissertations -- Aeronautics
dc.titleSupersonic, four shock, ramp type intake design, with internal boundary layer bleed
dc.typeThesis
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