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

Thesis (M. Eng. (Aeronautics)) -- University of Stellenbosch, 1990.

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Bibliographic Details
Main Author: Van Staden, Paul Arnold
Other Authors: Stellenbosch University. Faculty of . Dept. of .
Format: Thesis
Language:en_ZA
Published: Stellenbosch : Stellenbosch University 2012
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access_status_str Open Access
author Van Staden, Paul Arnold
author2 Stellenbosch University. Faculty of . Dept. of .
author_browse Stellenbosch University. Faculty of . Dept. of .
Van Staden, Paul Arnold
author_facet Stellenbosch University. Faculty of . Dept. of .
Van Staden, Paul Arnold
author_sort Van Staden, Paul Arnold
collection Thesis
dc_rights_str_mv Stellenbosch University
description Thesis (M. Eng. (Aeronautics)) -- University of Stellenbosch, 1990.
format Thesis
id oai:scholar.sun.ac.za:10019.1/68986
institution Stellenbosch University (South Africa)
language en_ZA
last_indexed 2026-06-10T12:44:34.165Z
license_str Other — see source repository
provenance_str_mv Harvested via OAI-PMH from SUNScholar — Stellenbosch University Repository
publishDate 2012
publishDateRange 2012
publishDateSort 2012
publisher Stellenbosch : Stellenbosch University
publisherStr Stellenbosch : Stellenbosch University
record_format dspace
source_str SUNScholar — Stellenbosch University Repository
spelling oai:scholar.sun.ac.za:10019.1/68986 Supersonic, four shock, ramp type intake design, with internal boundary layer bleed Van Staden, Paul Arnold Stellenbosch University. Faculty of . Dept. of . Gas-turbines -- Aerodynamics Aircraft gas-turbines -- Design and construction Airplanes -- Ramjet engines -- Air intakes Dissertations -- Aeronautics Thesis (M. Eng. (Aeronautics)) -- University of Stellenbosch, 1990. Full text to be digitised and attached to bibliographic record. 2012-08-27T12:26:52Z 2012-08-27T12:26:52Z 1990 Thesis http://hdl.handle.net/10019.1/68986 en_ZA Stellenbosch University 107 p. : ill. Stellenbosch : Stellenbosch University
spellingShingle Gas-turbines -- Aerodynamics
Aircraft gas-turbines -- Design and construction
Airplanes -- Ramjet engines -- Air intakes
Dissertations -- Aeronautics
Van Staden, Paul Arnold
Supersonic, four shock, ramp type intake design, with internal boundary layer bleed
title Supersonic, four shock, ramp type intake design, with internal boundary layer bleed
title_full Supersonic, four shock, ramp type intake design, with internal boundary layer bleed
title_fullStr Supersonic, four shock, ramp type intake design, with internal boundary layer bleed
title_full_unstemmed Supersonic, four shock, ramp type intake design, with internal boundary layer bleed
title_short Supersonic, four shock, ramp type intake design, with internal boundary layer bleed
title_sort supersonic four shock ramp type intake design with internal boundary layer bleed
topic Gas-turbines -- Aerodynamics
Aircraft gas-turbines -- Design and construction
Airplanes -- Ramjet engines -- Air intakes
Dissertations -- Aeronautics
url http://hdl.handle.net/10019.1/68986
work_keys_str_mv AT vanstadenpaularnold supersonicfourshockramptypeintakedesignwithinternalboundarylayerbleed