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Europe
 

T. Cain, D. Boyd (1999) Electroaerodynamics and the Effect of an Electric Discharge on Cone/Cylinder Drag at Mach 5. AIAA-99-0602, 37th Aerospace Sciences Meeting and Exhibit, Reno, Nevada.
 


 

Russia
 

E. Sheikin (2005) Parametric and Numerical Investigations of Scramjet with MHD Bypass. AIAA-2005-1336, 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada.
 

E. Sheikin, A. Kuranov (2005) MHD Control in Hypersonic Aircraft. AIAA-2005-1335, 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada.
 

V. V. Gogosov, N. L. Farber (1972) Equations of the electrohydrodynamics of multiphase media one-dimensional flows, discontinuous solutions, and damping of weak waves. Fluid Dynamics, Vol. 7, No. 5, pp. 751-762.
 


 

USA
 

M. Shneider, S. Macharet (2005) Hypersonic Aerodynamic Control and Thrust Vectoring by Nonequilibrium Cold-Air MHD Devices. AIAA-2005-979,
43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada.
 

M. Shneider, S. Macheret (2004) Modeling of Plasma Virtual Shape Control of Ram/Scramjet Inlet and Isolator. AIAA-2004-2662, 35th AIAA Plasmadynamics and Lasers Conference, Portland, Oregon.
 

S. O. Macheret, M. N. Shneider, G. V. Candler, R. W. Moses, J. F. Kline (2004) Magnetohydrodynamic Power Generation for Planetary Entry Vehicles. AIAA-2004-2560, 35th AIAA Plasmadynamics and Lasers Conference, Portland, Oregon.
 

D. Van Wie, A. Nedungadi (2004) Plasma Aerodynamic Flow Control for Hypersonic Inlets. AIAA-2004-4129, 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Fort Lauderdale, Florida.
 

Z. Li, C. Hawk (2002) Experimental Investigation of A Rectangular Shape Laboratory-Model Hall Current MHD Accelerator. AIAA-2002-3804, 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, Indiana.
 

H.-M. Damevin, K. A. Hoffmann (2002) Numerical Simulations of Magnetic Flow Control in Hypersonic Chemically Reacting Flows. Journal of Thermophysics and Heat Transfer, Vol. 16, No. 4, pp. 498-507. 
 

M. L. Spearman (1985) The Application of some Lifting-Body Reentry Concepts to Missile Design. AIAA-1985-497, 23rd AIAA Aerospace Sciences Meeting, Reno, Nevada.
 

S. T. Demetriades, C. D. Maxwell (1984) Strong MHD Interaction. AIAA-1984-155, 22nd AIAA Aerospace Sciences Meeting, Reno, Nevada.
 

C.-Y. Yoo, R. W. Porter (1973) Numerical analysis of the viscous, hypersonic, MHD blunt-body problem. AIAA Journal, Vol. 11, No. 3, pp. 383-384.
 

J. F. Coakley, R. W. Porter (1971) Time-Dependent Numerical Analysis of MHD Blunt Body Problem. AIAA Journal, Vol. 9, No. 8, pp. 1624-1626.
 

D. S. Miller, H. W. Carlson (1971) Application of Heat and Force Fields to Sonic-Boom Minimization. Journal of Aircraft, Vol. 8, No. 8, pp. 657-662.
 

D. S. Miller, H. W. Carlson (1970) On the Application of Heat and Force Fields to the Sonice Boom Minimization Problem. AIAA-1970-903, 2nd AIAA Aircraft Design and Operations Meeting, Los Angeles, California.
 

D. Siegelman (1970) Sonic Boom Minimization Schemes. Journal of Aircraft, Vol. 7, No. 3, pp. 280-281.
 

M. S. Cahn, C. M. Andrew, W. E. Anderson (1970) Recent Experiments in Supersonic Regime with Electrostatic Charges. AIAA-1970-759, 3rd AIAA Fluid and Plasma Dynamics Conference, Los Angeles, California.
 

S.-I. Cheng, A. Goldburg (1969) An Analysis of the Possibility of Reduction of Sonic Boom by Electro-Aerodynamic Devices. AIAA-1969-38.
 

M. S. Cahn, G. M. Andrew (1968) Electroaerodynamics in Supersonic Flow. AIAA-1968-24, 6th Aerospace Sciences Meeting, New York, NY.
 

R. W. Porter (1968) Aerodynamic Configurations Yielding Lift Without Sonic Boom. Journal of Aircraft, Vol. 5, No. 6, pp. 606-607.
 

R. W. Porter, A. B. Cambel (1967) Hall Effect in Flight Magnetogasdynamics. AIAA Journal, Vol. 5, No. 12, pp. 2208-2213.
 

R. Nowak, S. Kranc, R. W. Porter, M. C. Yuen, A. B. Cambel (1967) Magnetogasdynamic Re-entry Phenomena. J. Spacecraft, Vol. 4, No. 11, pp. 1538-1542.
 

R. W. Porter, A. B. Cambel (1967) Magnetic Coupling in Flight Magnetoaerodynamics. AIAA Journal, Vol. 5, No. 4, pp. 803-805.
 

S. Kranc, R. W. Porter, A. B. Cambel (1967) Electrodeless Magnetogasdynamic Power during Entry. J. Spacecraft, Vol 4, No. 6, pp. 813-815.
 

S. Selamoglu (1967) Experiments on Joule Heating of Shock-Ionizd Air. AIAA Journal, Vol. 5, No. 5, pp. 847-852.
 

R. L. Leonard, J. A. Fay (1965) Experiments on a Quasi-steady j x b Accelerator. AIAA Journal, Vol. 3, No. 1, pp. 115-121.
 

N. A. Jaffe (1966) Effects of a Transverse Magnetic Field and Spanwise Electric Field on the Boundary Layer of a Conducting Fluid. AIAA Journal, Vol. 4, No. 10, pp. 1843-1846.
 

R. H. Levy, P. J. Gierasch, D. B. Henderson (1964) Hypersonic Magnetohydrodynamics with or without a Blunt Body. AIAA Journal, Vol. 2, No. 12, pp. 2091-2099.
 

M. R. El-Saden (1962) A Class of Linear Magnetohydrodynamic Flows. AIAA Journal, Vol. 1, No. 1, pp. 236-238.
 

C. F. Knopp, C. F. Gottschlich, A. B. Cambel (1962) The spectroscopic measurement of temperature in transparent argon plasmas. J. Quant. Spectrosc. Radiat. Transfer, Vol. 2, pp. 297-299.
 

S. T. Demetriades (1962) Experiments with a High Specific Impulse Crossed-Field Accelerator. NSL-62-130, Northrop Space Labs, Northrop Corp. Presented at Third Symposium on Engineering Aspects of Magnetohydrodynamics, University of Rochester.
 

S. T. Demetriades, G. L. Hamilton, R. W. Ziemer, P. D. Lenn (1962) Three-Fluid Non-Equilibrium Plasma Accelerators, Part 1, ARS Preprint 2375-62.
 

S. T. Demetriades (1960) Experimental Magnetohydrodynamic Engine for Argon, Nitrogen and Air. ASRL-TM-60-23, Norair Div., Nothrop Corp. Presented at Second Symposium on Engineering Aspects of MHD, Columbia University, pp. 19-44.
 

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