Computational Study on the Design Parameters of S-Type Subsonic Inlets-Reference-Cited by-同舟云学术

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Computational Study on the Design Parameters of S-Type Subsonic Inlets

Published:2008-01-07 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Basoglu Osman¹,Yalcin Levent¹,Yilmaz Ali¹

Affiliation:

1. TUBITAK-SAGE

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-73

Reference6 articles.

1. 1Goldsmith,E.andSeddon,J.,editors,PracticalIntakeAerodynamicDesign,AIAAEducationSeries,AmericanInstitute of Aeronauticsand Astronautics,Washington, DC, 1993.

2. 2Lacau,R.,Garnero,P.,andGaible,F."ComputationofSupersonicInlets",AGARDSpecialCourseonMissile Aerodynamics,AGARD Report 804, 1994.

3. 3Haas,M.,Elmquist,R.,andSobel,D."NAWCInletDesignandAnalysis(NIDA)Code,"Tech.Rep.UTRCReport R92-970037-1,UnitedTechnologies ResearchCenter, April 1992.

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2. Application of Response Surface Methodology to Optimize Aerodynamic Performance of NACA Inlet;53rd AIAA/SAE/ASEE Joint Propulsion Conference;2017-07-07

3. Numerical Analysis of Effect of Boundary Layer Characteristics on the Flow Field in S-shaped Inlet;MATEC Web of Conferences;2015

4. Numerical investigation of centerline curvature effects on a compact S-shaped intake;Journal of Thermal Science;2012-09-07

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