Investigation of a flow around cavitiesSHVETS, A. I.Journal of engineering physics and thermophysics. 2003, Vol 76, Num 6, pp 1208-1214, issn 1062-0125, 7 p.Article

Supersonic moist air flow with condensation in a wavy wall channelKWON, Soon-Bum; AHN, Hyung-Joon.KSME international journal. 2001, Vol 15, Num 4, pp 492-499, issn 1226-4865Article

Histoire d'un transfert de technologie de l'aéronautique à la chimie = A technology transfer from aeronautics to chemistryTechnologies France (Strasbourg). 2001, Num 72, pp 2-4, issn 1257-2489, 5 p.Article

Completely parallel compressible flow simulations using adaptive unstructured meshesLEYLAND, P; RICHTER, R.Computer methods in applied mechanics and engineering. 2000, Vol 184, Num 2-4, pp 467-483, issn 0045-7825Article

Effect of the plenum-chamber diameter on the turbulent characteristics of a supersonic jetMAL'TSEV, V. A; NOVOPASHIN, S. A; PEREPELKIN, A. L et al.Journal of applied mechanics and technical physics. 1999, Vol 40, Num 6, pp 1057-1060, issn 0021-8944Article

Prandtl-Meyer expansion of a mixture of gases with a large disparity in molecular massesDOLGUSHEV, S. V; FOMIN, V. M.Journal of applied mechanics and technical physics. 1997, Vol 38, Num 1, pp 58-63, issn 0021-8944Article

Etude expérimentale d'une couche de mélange turbulente supersonique et analyse des propriétés de similitude = Experimental study of a turbulent supersonic mixing layer and analysis of the similarity propertiesMenaa, Mohamed; Dussauge, Jean-Paul.1997, 150 p.Thesis

Analysis of unsteady supersonic cavity flow employing an adaptive meshing algorithmXIN ZHANG; EDWARDS, J. A.Computers & fluids. 1996, Vol 25, Num 4, pp 373-393, issn 0045-7930Article

Performance of a hypersonic twin-nozzle systemBEYLICH, A. E.AIAA journal. 1996, Vol 34, Num 5, pp 953-960, issn 0001-1452Article

Velocity and turbulence measurements in a supersonic base flow with mass bleedMATHUR, T; DUTTON, J. C.AIAA journal. 1996, Vol 34, Num 6, pp 1153-1159, issn 0001-1452Conference Paper

A high-order streamline Godunov scheme for steady supersonic flow computationHSU, C. A; YANG, J. Y.Computer methods in applied mechanics and engineering. 1995, Vol 124, Num 4, pp 283-302, issn 0045-7825Article

Dense gas flow in minimum length nozzlesALDO, A. C; ARGROW, B. M.Journal of fluids engineering. 1995, Vol 117, Num 2, pp 270-276, issn 0098-2202Article

A Biot-Savart type formula for supersonic flowJADIC, I.Zeitschrift für angewandte Mathematik und Mechanik. 1994, Vol 74, Num 5, pp T462-T464, issn 0044-2267Article

Numerical solution of the problem of shock tube flow development with transverse diaphragm withdrawalVASIL'EV, E. I; DANIL'CHUK, E. V.Fluid dynamics. 1994, Vol 29, Num 2, pp 270-276, issn 0015-4628Article

Penetration and mixing of gas jets in supersonic cross flowBILLIG, F. S; SCHETZ, J. A.AIAA journal. 1994, Vol 32, Num 7, pp 1533-1535, issn 0001-1452Article

The pattern and restructuring of supersonic flow past a pair of bodiesKHLEBNIKOV, V. S.Fluid dynamics. 1994, Vol 29, Num 1, pp 123-128, issn 0015-4628Article

Analytical study of supersonic isentropic flow in a channel of constant cross section and an adjacent Laval nozzle. Comparison with numerical and experimental resultsPIRUMOV, U. G.Fluid dynamics. 1994, Vol 29, Num 4, pp 567-576, issn 0015-4628Article

A difference scheme of quasicharacteristics and its use to calculate supersonic gas flowLEVIN, M. P.Computational mathematics and mathematical physics. 1993, Vol 33, Num 1, pp 113-121, issn 0965-5425Article

On the free unsteady expansion of an ideal gasKRAIKO, A. N.Fluid dynamics. 1993, Vol 28, Num 4, pp 553-559, issn 0015-4628Article

Calcul des couches limites tridimensionnelles hypersoniques par une méthode de caractéristique. Approches classique et déficitaire = Computation of 3D hypersonic boundary layers by a characteristic method. Conventional and defect approachesCORJON, A; AUPOIX, B.La Recherche aérospatiale. 1993, Num 6, pp 9-26, issn 0034-1223Article

Analyse des perturbations induites par les couches limites des parois latérales d'une soufflerie sur un profil en régime transsonique = Analysis of perturbations induced by the wind tunnel sidewall boundary layer on an airfoil in transonic flowsMichonneau, Jean-François; Mignosi, André.1993, 200 p.Thesis

Study on supersonic flow past a pointed bodySHUXING CHEN.International series of numerical mathematics. 2001, pp 237-245, issn 0373-3149, isbn 3-7643-6711-3Conference Paper

Pressure over a dual-cavity cascade at supersonic speedsZHANG, X; EDWARDS, J. A.Aeronautical Journal. 1999, Vol 103, Num 1019, pp 45-54, issn 0001-9240Article

Analysis of action of a local source of energy on a supersonic flow around an elliptic coneKOROTAEVA, T. A; FOMIN, V. M; SHASHKIN, A. P et al.Journal of applied mechanics and technical physics. 1999, Vol 40, Num 6, pp 1016-1019, issn 0021-8944Article

Formation of a petal-shaped structure at tide front of an axisymmetric liquid film induced by collision of a drop with a flat surfaceFEDORCHENKO, A. I; CHERNOV, A. A.Journal of applied mechanics and technical physics. 1999, Vol 40, Num 6, pp 1077-1081, issn 0021-8944Article