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Performance analysis of a scramjet inlet-isolator using experimental and numerical methods

Performance analysis of a scramjet inlet-isolator using experimental and numerical methods
Performance analysis of a scramjet inlet-isolator using experimental and numerical methods
Experimental and numerical investigations were conducted to understand the complex flow features inside a generic two dimensional planar scramjet inlet-isolator. The inlet-isolator was designed to satisfy the ideal condition of Shock-on-Lip (SOL) in Mach 5 inviscid flow. Angle of attack was varied to simulate offdesign flight conditions for the inlet-isolator. Numerical methods were used to estimate various performance indicators at different test conditions. The changes in inlet efficiencies were shown to be heavily influenced on the flow quality inside the isolator.
2907 - 2915
International Council of the Aeronautical Sciences
Idris, A.C.
9772f9bc-206b-41a6-b631-081239ff552e
Saad, M.R.
ff1ed28c-a358-43e1-8ae1-fc1a0a5b2c5a
Zare-Behtash, H.
74be9b97-cb09-49c6-9f75-7ec58c0dd16c
Erdem, E.
e9f932d8-a17d-43d4-88cc-b46cfbecc64c
Kontis, K.
e40ecdbc-e5e9-4522-abf9-e3c3f3c2d7fa
Idris, A.C.
9772f9bc-206b-41a6-b631-081239ff552e
Saad, M.R.
ff1ed28c-a358-43e1-8ae1-fc1a0a5b2c5a
Zare-Behtash, H.
74be9b97-cb09-49c6-9f75-7ec58c0dd16c
Erdem, E.
e9f932d8-a17d-43d4-88cc-b46cfbecc64c
Kontis, K.
e40ecdbc-e5e9-4522-abf9-e3c3f3c2d7fa

Idris, A.C., Saad, M.R., Zare-Behtash, H., Erdem, E. and Kontis, K. (2012) Performance analysis of a scramjet inlet-isolator using experimental and numerical methods. In 28th Congress of the International Council of the Aeronautical Sciences 2012, ICAS 2012. International Council of the Aeronautical Sciences. 2907 - 2915 .

Record type: Conference or Workshop Item (Paper)

Abstract

Experimental and numerical investigations were conducted to understand the complex flow features inside a generic two dimensional planar scramjet inlet-isolator. The inlet-isolator was designed to satisfy the ideal condition of Shock-on-Lip (SOL) in Mach 5 inviscid flow. Angle of attack was varied to simulate offdesign flight conditions for the inlet-isolator. Numerical methods were used to estimate various performance indicators at different test conditions. The changes in inlet efficiencies were shown to be heavily influenced on the flow quality inside the isolator.

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Published date: 2012

Identifiers

Local EPrints ID: 493507
URI: http://eprints.soton.ac.uk/id/eprint/493507
PURE UUID: b56f4855-698d-444a-940f-b697b5d737a0
ORCID for H. Zare-Behtash: ORCID iD orcid.org/0000-0002-4769-4076

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Date deposited: 04 Sep 2024 16:40
Last modified: 05 Sep 2024 02:07

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Contributors

Author: A.C. Idris
Author: M.R. Saad
Author: H. Zare-Behtash ORCID iD
Author: E. Erdem
Author: K. Kontis

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