Applications

Joseph J. S. Shang; Sergey T. Surzhikov

doi:10.1017/9781108292566.011

10 - Applications

Published online by Cambridge University Press: 20 June 2018

Joseph J. S. Shang and

Sergey T. Surzhikov

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Joseph J. S. Shang: Affiliation:
Wright State University, Ohio
Sergey T. Surzhikov: Affiliation:
Russian Academy of Sciences, Moscow

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Type: Chapter
Information: Plasma Dynamics for Aerospace Engineering , pp. 342 - 382

DOI: https://doi.org/10.1017/9781108292566.011 [Opens in a new window]

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. 1–13.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. 256–269.CrossRef Google Scholar

Barthelemy, R.R., The National Aero-Space Plane program, AIAA 1989–5053, July 1989.CrossRef Google Scholar

Beam, R.M. and Warming, R.F., An implicit factored scheme for the compressible Navier-Stokes equations, AIAA J., Vol. 16, 1978, pp. 393–401.CrossRef Google Scholar

Bird, B.B., Stewart, W.E., and Lightfoot, E.N., Transport phenomena (2nd edn.), John Wiley & Sons, New York, 2002, pp. 515–860.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.CrossRef Google 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. 2450–2463.Google Scholar

Bush, W.B., Magnetohydrodynamic-hypersonic flow past a blunt body, J. Aerosp. Sci., Vol. 25, Nov. 1958, pp. 685–690, 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. 475–483.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. 961–970.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. 193–217.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. 1063–1077.CrossRef Google 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. 589–594.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. 923–925.Google Scholar

Gaitonde, D.V., Magnetohydrodynamic energy-bypass procedure in a three-dimensional scramjet, J. Propul. Power, Vol. 22, No. 2, 2006, pp. 498–510.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. 262–268.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. 1–7.CrossRef Google 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. 514–667.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. 1185–1195.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. 19–38.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. 741–752.CrossRef Google 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.CrossRef Google 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. 442–462.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. 76–90.CrossRef Google Scholar

Park, C., Stagnation-point radiation for Apollo 4, J. Thermophys. Heat Transfer, Vol. 18, 2004, pp. 348–357.Google Scholar

Park, C., Calculation of stagnation-point heating rates associated with Stardust vehicle, J. Spacecr. Rockets, Vol. 44, No. 1, 2007, pp. 24–32.Google Scholar

Park, C. and Balakrishnan, A., Ablation of Galileo probe heat-shield models in a ballistic range, AIAA J., Vol. 23, 1985, pp. 301–308.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. 804–813.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. 311–349.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. 1178–1186.CrossRef Google 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. 2710–2720.CrossRef Google 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.CrossRef Google Scholar

Shang, J.S. and Surzhikov, S.T., Simulating nonequilibrium flow for ablating Earth reentry, J. Spacecr. Rockets, Vol. 47, No. 5, 2010, pp. 806–816.Google Scholar

Shang, J. and Surzhikov, S.T., Simulating Stardust reentry with radiation reentry, J. Spacecr. Rockets, Vol. 48, No. 3, 2011, pp. 385–396.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. 642–668.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. 302–309.Google Scholar

Starikovskaia, S.M., Plasma assisted ignition and combustion, J. Phys. D Appl. Phys., Vol. 39, 2006, pp. R265–R299.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. 875–888.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. 70–92.Google Scholar

Thomas, F., Kozlov, A., and Corke, T., Plasma actuators for bluff body flow control, AIAA J., Vol. 46, 2008, pp. 1921–1931.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. 1022–1026.CrossRef Google Scholar

Verboncoeur, J.P., Particle simulation of plasmas: Review and advances, Plasma Phys. Control Fusion, Vol. 47, 2005, A231–260.CrossRef Google 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. 1603–1609.Google Scholar

Ziemer, R.W., Experimental investigation in magneto-aerodynamics, J. Am. Rocket Soc., Vol. 29, 1959, pp. 642–647.Google Scholar

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10 - Applications

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