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Volumn 16, Issue , 2006, Pages 12067-12081

Plasma-based control of shock-wave / boundary-layer interaction

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; BOUNDARY LAYERS; COMPUTATIONAL METHODS; PLASMAS; THERMAL GRADIENTS;

EID: 34250698015     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-1007     Document Type: Conference Paper
Times cited : (8)

References (33)
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  • 15
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    • Poggie, J., "Numerical Exploration of Flow Control with Glow Discharges," AIAA Paper 2004-2658, American Institute of Aeronautics and Astronautics, Reston VA, June 2004.
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    • Poggie, J.1
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    • Transition from the Constant Ion Mobility Regime to the Ion-Atom Charge-Exchange Regime for Bounded Collisional Plasmas
    • Feb
    • Poggie, J. and Sternberg, N., "Transition from the Constant Ion Mobility Regime to the Ion-Atom Charge-Exchange Regime for Bounded Collisional Plasmas," Physics of Plasmas, Vol. 12, No. 2, Feb. 2005.
    • (2005) Physics of Plasmas , vol.12 , Issue.2
    • Poggie, J.1    Sternberg, N.2
  • 19
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    • Holden, M. S. and Moselle, J. R., Theoretical and Experimental Studies of the Shock Wave - Boundary Layer Interaction on Compression Surfaces in Hypersonic Flow, Tech. Rep. ARL 70-0002, Aerospace Research Laboratories, January 1970.
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    • Beam, R.1    Warming, R.2
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    • Pulliam, T. H., "Implicit Finite-Difference Simulations of Three-Dimensional Compressible Flow," AIAA Journal, Vol. 18, No. 2, 1980, pp. 159-167.
    • (1980) AIAA Journal , vol.18 , Issue.2 , pp. 159-167
    • Pulliam, T.H.1
  • 27
    • 0016941891 scopus 로고
    • Numerical Solutions of Supersonic and Hypersonic Laminar Compression Ramp Flows
    • Hung, C. M. and MacCormack, R. W., "Numerical Solutions of Supersonic and Hypersonic Laminar Compression Ramp Flows," AIAA Journal, Vol. 14, No. 4, 1976, pp. 475-481.
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  • 28
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    • Computation of Laminar Hypersonic Compression-Corner Flows
    • Rudy, D. H., Thomas, J. L., Kumar, A., Gnoffo, P. A., and Chakravarthy, S. R., "Computation of Laminar Hypersonic Compression-Corner Flows," AIAA Journal, Vol. 29, No. 7, 1991, pp. 1108-1113.
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.