Evaluation of Turbulence Model Corrections for Supersonic Jets Using the OVERFLOW Code-Reference-Cited by-同舟云学术

Evaluation of Turbulence Model Corrections for Supersonic Jets Using the OVERFLOW Code

Published:2010-06-28 Issue: Volume: Page:
ISSN:
Container-title:40th Fluid Dynamics Conference and Exhibit
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Author:

Gross Nico¹,Blaisdell Gregory¹,Lyrintzis Anastasios¹

Affiliation:

1. Purdue University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4604

Reference18 articles.

1. 1Nichols,R.H.andBuning,P.G.,User’sManualforOVERFLOW2.1-Version2.1t,August2008.

2. 2NASAConstellationMultimedia,[online],http://www.nasa.gov/missionpages/constellation/multimedia/index.html[retreivedJuly17,2009].

3. 3Eggers, J. E. “Velocity profiles and eddy viscosity distributions downstream of a Mach 2.22 nozzle exhausting into quiescent air,” Tech. rep.,NASATND-3601,1966.

4. 4Birch,F.andEggers,J.E.“Acriticalreviewoftheexperimentaldataonturbulentshearlayers,”Tech.rep.,NASASP321,1972.

5. Measurements in subsonic and supersonic free jets using a laser velocimeter

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