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10 - Applications

Published online by Cambridge University Press:  20 June 2018

Joseph J. S. Shang
Affiliation:
Wright State University, Ohio
Sergey T. Surzhikov
Affiliation:
Russian Academy of Sciences, Moscow
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Publisher: Cambridge University Press
Print publication year: 2018

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References

Adamovich, I.V., Choi, I., Jiang, N., Kim, J.-H., Keshav, S., Lempert, W.R., Mntusov, E., Nishihara, M., Samimy, M., and Uddi, M., Plasma assisted ignition and high-speed flow control: Non-thermal and thermal effects, Plasma Source Sci. Technol., Vol. 18, 2009, pp. 113.Google Scholar
Adelgren, R.G., Yan, H., Elliott, G.S., Knight, D.D., Beutner, T.J., and Zheltovodov, Z.A., Control of Edney, IV interaction by pulsed laser energy deposition, AIAA J., Vol. 43, No. 2, 2005, pp. 256269.CrossRefGoogle Scholar
Barthelemy, R.R., The National Aero-Space Plane program, AIAA 1989–5053, July 1989.CrossRefGoogle Scholar
Beam, R.M. and Warming, R.F., An implicit factored scheme for the compressible Navier-Stokes equations, AIAA J., Vol. 16, 1978, pp. 393401.CrossRefGoogle Scholar
Bird, B.B., Stewart, W.E., and Lightfoot, E.N., Transport phenomena (2nd edn.), John Wiley & Sons, New York, 2002, pp. 515860.Google Scholar
Birdsall, C.K. and Langdon, A.B., Plasma physics via computer simulation, McGraw-Hill, Singapore, 1985.Google Scholar
Bityurin, V.A., Linberry, J.T., Litchford, R.J., and Cole, J.W., Thermodynamic analysis of the AJAX propulsion concept, AIAA Preprint 2000–0445, Reno NV, 2000.Google Scholar
Bletzinger, P., Ganguly, B.N., Van Wie, D., and Garscadden, A., Plasma in high-speed aerodynamics, J. Phys. D Appl. Phys., Vol. 38, 2005, pp. R33–57.CrossRefGoogle Scholar
Boeuf, J.P. and Pitchford, L.C., Electrohydrodynamic force and aerodynamic flow acceleration in surface dielectric barrier discharge, J. Appl. Phys., Vol. 97, 2005, pp. 103307-1-10.Google Scholar
Borghi, C.A., Carraro, M.R., Cristofolini, A., Veefkind, A., Baigioni, L., Fantoni, G., Passaro, A., Capitelli, M., and Colonna, G., Magnetohydrodynamic interaction in the shock layer of a wedge in hypersonic flow, IEEE Trans. Plasma Sc., Vol. 34, 2006, pp. 24502463.Google Scholar
Bush, W.B., Magnetohydrodynamic-hypersonic flow past a blunt body, J. Aerosp. Sci., Vol. 25, Nov. 1958, pp. 685690, 728.Google Scholar
Cauchon, D.L., Radiative heating results from the Fire II flight experiment at a reentry velocity of 11.4 km/s, 1967. NASA TM-X-1402.Google Scholar
Cheatwood, F. and Gnoffo, P., User’s manual for the Langley aerothermodynamic upwind relaxation algorithm (LAURA), NASA TM, 4674, Apr. 1996.Google Scholar
Chen, Y.K., and Milos, F.S., Ablation and thermal response program for spacecraft heatshield analysis, J. Spacecr. Rockets, Vol. 36, 1999, pp. 475483.Google Scholar
Chen, Y.K. and Milos, F.S., Navier-Stokes solutions with finite rate ablation for planetary mission Earth reentries, J. Spacecr. Rockets, Vol. 42, No. 6, 2005, pp. 961970.Google Scholar
Corke, T.C., Post, M.L., and Orlov, D.M., SDBD plasma enhanced aerodynamics: concepts, optimization and applications, Prog. Aerosp. Sci., Vol. 43, 2007, pp. 193217.Google Scholar
Currant, E.T. and Murthy, S.N.B., Scramjet propulsion, AIAA Prog. Astronaut. Aeronaut., Vol. 189, New York, 2001.Google Scholar
Cybulski, R.J., Domino, E.J., Kotnik, J.T., Lovell, R.R., and Shellhammer, D.M., Results from CERT1 in rocket flight test, NASA TN-2718, Lewis Research Center, Cleveland, OH, 1966.Google Scholar
Dunn, M.G. and Kang, S.W., Theoretical and experimental studies of reentry plasma, NSA CR 2232, April 1973.Google Scholar
Elisson, B. and Kogelschatz, U., Nonequilibrium volume plasma chemical processing, IEEE Trans. Plasma Sci., Vol. 19, 1991, pp. 10631077.CrossRefGoogle Scholar
Enloe, C.L., McLaughlin, T.E., Van Dyken, R.D., Kachner, K.D., Jumper, E.J., and Corke, T.C., Mechanisms and responses of a single dielectric barrier plasma actuator: Plasma morphology, AIAA J. Vol. 42, 2004, pp. 589594.Google Scholar
Fraishtadt, V.L., Kuranov, A.L., and Sheikin, E.G., Use of MHD systems in hypersonic aircraft, Tech. Physics, Vol. 43, No. 11, 1998, p. 1309.Google Scholar
Fredrick, R.A., Blevins, J.A., and Coleman, H.W., Investigation of microwave attenuation measurements in a laboratory-scale motor plume, J. Spacecr. Rockets, Vol. 32, No. 5, 1995, pp. 923925.Google Scholar
Gaitonde, D.V., Magnetohydrodynamic energy-bypass procedure in a three-dimensional scramjet, J. Propul. Power, Vol. 22, No. 2, 2006, pp. 498510.Google Scholar
Gallimore, A., Meyer, R., Kelley, A., and Jahn, R. Anode power deposition in applied-field segmented anode MPD thruster, J. Propul. Power, Vol. 10, 1994, pp. 262268.Google Scholar
Ganiev, Y.C., Gordeev, V.P., Krasilnikov, A.V., Lagutin, V.I., Otmennikov, V.N., and Panasenko, A.V., Aerodynamic drag reduction by plasma and hot-gas injection. J. Thermophys. Heat Transfer, 2000, Vol. 14, No. 1, pp. 17.CrossRefGoogle Scholar
Gurijanov, E.P. and Harsha, P.T., Ajax: New directions in hypersonic technology, AIAA J., 1996–4609, Nov. 1996.Google Scholar
Hayes, W.D. and Probstein, R.F., Hypersonic flow theory, Academic Press, New York, 1959.Google Scholar
Hirschfelder, J.O., Curtiss, C.F., and Bird, B.B., Molecular theory of gases and liquid (2nd printing), John Wiley & Sons, New York, 1954, pp. 514667.Google Scholar
Jacobsen, L.S., Carter, C.D., Jackson, T.A., and Baurle, R.A., Toward plasma-assisted ignition in scramjet, AIAA Preprint, 2003–0871, 2003.Google Scholar
Jahn, R.G., Physics of electric propulsion, McGraw-Hill, New York, 1968.Google Scholar
Johnston, C.O., Hollis, B.R., and Sutton, K., Nonequilibrium stagnation-line radiative heating for Fire-II, J. Spacecr. Rockets, Vol. 45, No. 6, 2008, pp. 11851195.Google Scholar
Kuo, K.K., Principles of combustion (2nd edn.), John Wiley & Sons, New York, 2005.Google Scholar
Law, C.K., Fuel options for the next generation chemical propulsion, AIAA J., Vol. 50, No. 1, 2012, pp. 1938.Google Scholar
Lieberman, M.A. and Lichtenberg, A.J., Principle of plasma discharges and materials processing, John Wiley & Sons, New York, 2005.Google Scholar
Liu, Y., Prabhu, D., Trumble, K.A., Saunders, D., and Jenniskens, P., Radiation modeling for the reentry of the Stardust sample return capsule, J. Spacecr. Rockets, Vol. 47, No. 5, 2010, pp. 741752.CrossRefGoogle Scholar
Longmier, B., Squire, J., Carter, M., Cassady, L., Glover, T., Chancery, W., Olsen, C., Ilin, A., McCaskill, G., Chang Diaz, F.R., and Bering, E., Ambipolar ion acceleration in the expanding magnetic nozzle of the VASIMR VX-200i, AIAA Preprint, 2009–5359, 2009.Google Scholar
Mahalingam, S., Partile based plasma simulation for an ion engine discharge, Doctoral dissertation, Wright State University, Ohio, 2007.CrossRefGoogle Scholar
Meyer, R.C. On reducing aerodynamic heat transfer rates by magnetohydrodynamics techniques, J. Aero. Sci., Mar. 1958, pp. 561–566, 572.Google Scholar
Mitchner, M. and Kruger, C.H., Partially ionized gases, John Wiley & Sons, New York, 1973.Google Scholar
Olynick, D.R., Chen, Y.K., and Tauber, M.E., Aerodynamics of the Stardust sample return capsule, J. Spacecr. Rockets, Vol. 36, No. 3, 1999, pp. 442462.Google Scholar
Olynick, D.R., Henline, W.D., Hartung, L.C., and Candler, G.V., Comparison of coupled radiative Navier-Stokes flow solutions with the project Fire-II flight data, AIAA Preprint, 1994–1955, 1994.Google Scholar
Park, C. Chemical-kinetics parameters of hypersonic earth entry, J. Thermophys. Heat Transfer, 2001, Vol. 15, pp. 7690.CrossRefGoogle Scholar
Park, C., Stagnation-point radiation for Apollo 4, J. Thermophys. Heat Transfer, Vol. 18, 2004, pp. 348357.Google Scholar
Park, C., Calculation of stagnation-point heating rates associated with Stardust vehicle, J. Spacecr. Rockets, Vol. 44, No. 1, 2007, pp. 2432.Google Scholar
Park, C. and Balakrishnan, A., Ablation of Galileo probe heat-shield models in a ballistic range, AIAA J., Vol. 23, 1985, pp. 301308.Google Scholar
Petrusev, A.S., Surzhikov, S.T., and Shang, J.S., A two-dimensional model of glow discharge in view of vibrational excitation o molecular nitrogen, High Temp., Vol. 44, No. 6, 2006, pp. 804813.Google Scholar
Post, M.L., Plasma actuators for separation control on stationary and oscillating wings, PhD dissertation, University of Notre Dame, 2004.Google Scholar
Reshoko, E., Boundary-layer stability and transition, Annu. Rev. Fluid Mech., Vol. 8, 1976, pp. 311349.Google Scholar
Resler, E.L. and Sears, W.R., The prospects for magneto-aerodynamics. J. Aero. Sci., Vol. 25, 1958, pp. 235, 258.Google Scholar
Shang, J.S., Numerical simulation of hypersonic flows, Computational methods in hypersonic flow, Computational Mechanics Publications, South Hampton, UK, 1992.Google Scholar
Shang, J.S., Plasma injection for hypersonic blunt body drag reduction, AIAA J., Vol. 40, No. 6, 2002, pp. 11781186.CrossRefGoogle Scholar
Shang, J.S., Chang, C., and Surzhikov, S.T., Simulating hypersonic magneto-fluid dynamic compression in rectangular inlet, AIAA J., Vol. 45, No. 11, 2007, pp. 27102720.CrossRefGoogle Scholar
Shang, J.S., Roveda, F., and Huang, P.G., Electrodynamic force of dielectric barrier discharge, J. Appl. Phys., Vol. 109, No. 11. 2011, pp. 113301-1-8.CrossRefGoogle Scholar
Shang, J.S. and Surzhikov, S.T., Simulating nonequilibrium flow for ablating Earth reentry, J. Spacecr. Rockets, Vol. 47, No. 5, 2010, pp. 806816.Google Scholar
Shang, J. and Surzhikov, S.T., Simulating Stardust reentry with radiation reentry, J. Spacecr. Rockets, Vol. 48, No. 3, 2011, pp. 385396.Google Scholar
Shang, J.S., Surzhikov, S.T., Kimmel, R., Gaitonde, D., Menart, J., and Hayes, J., Mechanisms of plasma actuators for hypersonic flow control, Prog. Aerosp. Sci., Vol. 41, No. 8, Nov. 2005, pp. 642668.Google Scholar
Shang, J.S. Computational electromagnetic-aerodynamics, IEEE Press Series on RF and Microwave Technology, John Wiley & Sons, Hoboken, NJ, 2016.Google Scholar
Sharma, S., Shock front radiation measurements in air, AIAA Preprint 91–0573, 1991.Google Scholar
Smoot, L.D. and Underwood, D.L., Prediction of microwave attenuation characteristics of rocket exhausts, J. Spacecr. Rockets, Vol. 3, No. 3, 1966, pp. 302309.Google Scholar
Starikovskaia, S.M., Plasma assisted ignition and combustion, J. Phys. D Appl. Phys., Vol. 39, 2006, pp. R265R299.Google Scholar
Surzhikov, S.T., Computing system for mathematical simulation of selective radiation transfer, AIAA Preprint 2000–2369, 2000.Google Scholar
Surzhikov, S.T. Radiation modeling and spectral data. Lecture series 2002–07: Physico-Chemical Models for High Enthalpy and Plasma Flows. Von Karman Institute for Fluid Dynamics.Google Scholar
Surzhikov, S.T. and Shang, J.S., Coupled radiation-gasdynamic model for Stardust earth entry simulation, J. Spacecr. Rockets, Vol. 49, No. 5, 2012, pp. 875888.Google Scholar
Surzhikov, S.T. and Shang, J.S., Fire-II flight test data simulations with different physical-chemical kinetics data and radiation models, Front. Aerosp. Eng., Vol. 4, No. 2, 2015, pp. 7092.Google Scholar
Thomas, F., Kozlov, A., and Corke, T., Plasma actuators for bluff body flow control, AIAA J., Vol. 46, 2008, pp. 19211931.Google Scholar
Treanor, C.E. and Marrone, P.V., Effect of dissociation on the rate of vibrational relaxation, Phys. Fluids, Vol. 5., No. 9, 1962, pp. 10221026.CrossRefGoogle Scholar
Verboncoeur, J.P., Particle simulation of plasmas: Review and advances, Plasma Phys. Control Fusion, Vol. 47, 2005, A231–260.CrossRefGoogle Scholar
Wright, M.J., Candler, G.V., and Bose, D., Data-parallel line relaxation method for the Navier-Stokes equations, AIAA J. Vol. 36, Sept. 1998, pp. 16031609.Google Scholar
Ziemer, R.W., Experimental investigation in magneto-aerodynamics, J. Am. Rocket Soc., Vol. 29, 1959, pp. 642647.Google Scholar

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  • Applications
  • Joseph J. S. Shang, Wright State University, Ohio, Sergey T. Surzhikov, Russian Academy of Sciences, Moscow
  • Book: Plasma Dynamics for Aerospace Engineering
  • Online publication: 20 June 2018
  • Chapter DOI: https://doi.org/10.1017/9781108292566.011
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  • Applications
  • Joseph J. S. Shang, Wright State University, Ohio, Sergey T. Surzhikov, Russian Academy of Sciences, Moscow
  • Book: Plasma Dynamics for Aerospace Engineering
  • Online publication: 20 June 2018
  • Chapter DOI: https://doi.org/10.1017/9781108292566.011
Available formats
×

Save book to Google Drive

To save content items to your account, please confirm that you agree to abide by our usage policies. If this is the first time you use this feature, you will be asked to authorise Cambridge Core to connect with your account. Find out more about saving content to Google Drive.

  • Applications
  • Joseph J. S. Shang, Wright State University, Ohio, Sergey T. Surzhikov, Russian Academy of Sciences, Moscow
  • Book: Plasma Dynamics for Aerospace Engineering
  • Online publication: 20 June 2018
  • Chapter DOI: https://doi.org/10.1017/9781108292566.011
Available formats
×