Pulsed Injection Flow Control for Throttling in Supersonic Nozzles - A Computational Fluid Dynamics Design Study-Reference-Cited by-同舟云学术

Pulsed Injection Flow Control for Throttling in Supersonic Nozzles - A Computational Fluid Dynamics Design Study

Published:2007-06-15 Issue: Volume: Page:
ISSN:
Container-title:37th AIAA Fluid Dynamics Conference and Exhibit
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Author:

Baruzzini Dan¹,Domel Neal¹,Miller Daniel¹

Affiliation:

1. Lockheed Martin Aeronautics Company

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-4215

Reference14 articles.

1. Bender,E., Miller,D.N., Smith,B.,Yagel, P.,Vermeulen.,P.,Walker,S.,2000, "SimulationofPulsed InjectioninaCrossflowUsing3-DUnsteadyCFD," AIAA No.2000-2318.

2. The formation of ‘optimal’ vortex rings, and the efficiency of propulsion devices

3. Tillman,C.P."Enhancement ofTransonicAirfoli PerformanceUsingPulsedJets forSeparationControl ,"AIAANo.2001-0731.

4. McManus,K.,Magill,J."SeparationControl on Incompressibleand Compressible Flows UsingPulsedJets,"AIAA No.96-1948.

5. Gunter,F.L. andFarenholz,F.E.,1961,"Final Report onaStudyofRocket Thrust Control byGas Injection,"Massachusetts Institite ofTechnolog,Naval Supersonic Laboratory,Technical Report 448.

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