T. Alziary de Roquefort

Follow

Generating author description...

All published works
Action Title Year Authors
+ Numerical investigation of restricted shock separated flow in supersonic nozzle 2009 A. Shams
P. Comte
Stéphane Girard
A. Benyahia
T. Alziary de Roquefort
+ Joint European Effort Towards Advanced Rocket Thrust Chamber Technology 2005 Manuel Frey
Axel Preuß
Stève Girard
T. Alziary de Roquefort
Philippe Reijasse
Ralf Stark
Klaus Hannemann
Richard Schwane
David Perigo
Luca Boccaletto
+ Unsteadiness of Flow Separation and End-Effects Regime in a Thrust-Optimized Contour Rocket Nozzle 2003 Anh Thi Nguyen
Hugues Deniau
Stéphane Girard
T. Alziary de Roquefort
+ European Cooperation on Flow Separation Control 2002 Manuel Frey
Roland Rydén
T. Alziary de Roquefort
G. Hagemann
Polagnagu James
Thierry Kachler
P. Reijasse
Richard Schwane
Ralf Stark
+ Wall Pressure Fluctuations in an Over-Expanded Rocket Nozzle 2002 Anh Nguyen
Hugues Deniau
Stève Girard
T. Alziary de Roquefort
+ Self-maintained glow discharge in a hypersonic air flow 2000 В. М. Фомин
T. Alziary de Roquefort
A. V. Lebedev
A. I. Ivanchenko
+ PDF Chat Smooth leading edge transition in hypersonic flow 1999 Ludovic Le Gaillard
Emmanuel Bénard
T. Alziary de Roquefort
+ Numerical investigation of a three-dimensional turbulent shock/shock interaction 1998 N. Duquesne
T. Alziary de Roquefort
+ Numerical investigation of shock-shock interactions on a swept cylinder 1995 N. Duquesne
T. Alziary de Roquefort
+ FLOW VISUALIZATION AND HEAT TRANSFER MEASUREMENT IN A HYPERSONIC WIND TUNNEL 1992 Luigi de Luca
Gennaro Cardone
Giovanni Maria Carlomagno
D. Aymer de la Chevalerie
T. Alziary de Roquefort
+ Attempt to Evaluate the Computations for Test Case 6.1 - Cold Hypersonic Flow Past Ellipsoidal Shapes - 1991 W. Kordulla
Jacques Périaux
T. Alziary de Roquefort
+ Pseudospectral multi-domain method for incompressible viscous flow computation 1990 A. Farcy
T. Alziary de Roquefort
+ On the existence of multiple periodic solutions of the Boussinesq equations 1988 Patrick Le Quéré
T. Alziary de Roquefort
+ A semi-implicit spectral method for the solution of the Navier-Stokes equations for an incompressible viscous two-dimensional flow 1982 P. Le Queré
T. Alziary de Roquefort
Common Coauthors
Commonly Cited References
Action Title Year Authors # of times referenced
+ Flow separation and side-loads in rocket nozzles 1999 Manuel Frey
G. Hagemann
3
+ Appearance of Restricted Shock Separation in Rocket Nozzles 2002 G. Hagemann
Manuel Frey
W. Koschel
2
+ Numerical investigation of separated nozzle flows 1994 C. L. Chen
S. R. Chakravarthy
C. M. Hung
2
+ Wall Pressure Fluctuations in an Over-Expanded Rocket Nozzle 2002 Anh Nguyen
Hugues Deniau
Stève Girard
T. Alziary de Roquefort
2
+ The Calorimeter Nozzle Programme 2002 G. Hagemann
Roland Rydén
Manuel Frey
Ralf Stark
Jan Alting
2
+ Subscale Nozzle Testing at the P6.2 Test Stand 2000 Manuel Frey
Ralf Stark
Helmut Ciezki
F. Quessard
W. Kwan
2
+ Flow separation and side-load behavior of the Vulcain engine 1999 Manuel Frey
Michael Terhardt
G. Hagemann
2
+ Side-Load Phenomena in Highly Overexpanded Rocket Nozzles 2004 Jan Östlund
Tomas Damgaard
Manuel Frey
2
+ Assessment of turbulence models in overexpanded rocket nozzle flow simulations 1999 Jan Östlund
Mattias Jaran
2
+ Flow Separation Phenomena in Subscale Rocket Nozzles 2002 W. Kwan
Ralf Stark
2
+ Validation of the Unstructured DLR-TAU-Code for Hypersonic Flows 2002 A. Mäck
Volker Hannemann
1
+ Restricted Shock Separation in Rocket Nozzles 2000 Manuel Frey
G. Hagemann
1
+ Numerical Simulation of Laminar Hypersonic Flow past a Double-Ellipsoid 1991 Stefan Riedelbauch
1
+ Measurement of heat transfer with an infrared camera 1968 H. Thomann
B. Frisk
1
+ Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes 1997 Philip L. Roe
1
+ Experimental shock-wave interference heating on a cylinder at Mach 6and 8 1989 Allan R. Wieting
Michael Holden
1
+ Unsteadiness of Flow Separation and End-Effects Regime in a Thrust-Optimized Contour Rocket Nozzle 2003 Anh Thi Nguyen
Hugues Deniau
Stéphane Girard
T. Alziary de Roquefort
1
+ Technology Investigation for High Area Ratio Nozzle Concepts 2003 G. Hagemann
Axel Preuß
Frank Grauer
Joachim Kretschmer
Manuel Frey
Roland Rydén
Ralf Stark
David Zerjeski
1
+ Experimental and Analytical Design Verification of the Dual-Bell Concept 2002 G. Hagemann
Michael Terhardt
D. Haeseler
Manuel Frey
1
+ PDF Chat Flow Separation in Rocket Nozzles, a Simple Criteria 2005 Ralf Stark
1
+ Status of flow separation prediction in liquid propellant rocket nozzles 1974 R. H. Schmucker
1
+ P6.2 Cold Gas Test Facility For Simulation of Flight Conditions - Current Activities 2005 Klaus Schäfer
C. Böhm
Harald Kronmüller
Ralf Stark
Herbert Zimmermann
1
+ Stability and Transition in Compressible Attachment-Line Boundary-Layer Flow 1995 Ray-Sing Lin
Mujeeb R. Malik
1
+ Transient flow simulation of a compressed truncated perfect nozzle 2001 Masahiro Takahashi
Shuichi Ueda
Takeo Tomita
Mamoru Takahashi
Hiroshi Tamura
Kenji Aoki
1
+ Visualization of the formation of separation bubbles on a bell-shaped nozzle surface in relation to serious side-load 2001 Takeo Tomita
Mamoru Takahashi
Masahiro Takahashi
Shuichi Ueda
Hiroshi Tamura
Kenji Aoki
1
+ Unsteadiness and asymmetry of shock-induced separation in a planar two-dimensional nozzle - A flow description 1999 Philippe Reijasse
Bernard Corbel
Didier Soulevant
1
+ The physical origins of side loads in rocket nozzles 1999 Marcello Onofri
Francesco Nasuti
1
+ Flow separation and side-load behavior of truncated ideal rocket nozzles 2001 Michael Terhardt
G. Hagemann
Manuel Frey
1
+ Validation of Unsteady Turbulent Flow Predictions for Over-expanded Rocket Nozzle 2003 Richard Schwane
L. Torngren
Henry Wong
1
+ Analytical and experimental studies of shock interference heating in hypersonic flows 1973 J. W. Keyes
F. D. Hains
1
+ Some aspects of the flow near a swept attachment line with particular referenceto boundary layer transition 1978 D. I. A. Poll
1
+ Shock Patterns in the Plume of Overexpanded Rocket Nozzles 1999 Manuel Frey
1
+ Scalability Discussion for Rocket Nozzle Flows Based on Subscale and Full-Scale Testing 2002 G. Hagemann
Jan Alting
D. Preclik
1
+ Computational Flow Simulations of Overexpanded Rocket Nozzle Flowfields including Unsteady Effects 2002 P.L. Vuillermoz
Hadrien Lambaré
A. Enzian
P. Steinfeld
Laurent Lequette
1
+ Semi-Empirical Flow Separation Model for Subscale Nozzles 2002 P. Reijasse
J. Birkemeyer
1
+ Approximate Riemann solvers, parameter vectors, and difference schemes 1981 Philip L. Roe
1
+ Cold Gas Subscale Test Facility P6.2 at DLR Lampoldshausen 2002 Harald Kronmüller
Klaus Schäfer
Herbert Zimmermann
Ralf Stark
1
+ Étude théorique et expérimentale de la transition en écoulement bidimensionnel compressible 1989 F. Vignau
1
+ Viscous hypersonic shock-on-shock interaction on blunt cowl lips 1988 G. H. Klopfer
H. C. Yee
1
+ Shock Interference Bell Aerospace, Heating in Hypersonic Flows 1972 F. D. Hains
J. W. Keyes
1
+ Thin-layer approximation and algebraic model for separated turbulentflows 1978 Betty Baldwin
Harvard Lomax
1
+ Application of essentially nonoscillatory schemes to unsteady hypersonic shock-shock interference heating problems 1994 Xiaolin Zhong
1
+ Advanced Flow Visualisation Techniques in Cold Gas Subscale Nozzles, a Comparison 2003 Ralf Stark
Harald Kronmueller
David Zerjeski
B. Wagner
1
+ Unsteady Side Loads in a Thrust-Optimized Contour Nozzle at Hysteresis Regime 2004 Sébastien Deck
Anh Thi Nguyen
1
+ Correlations of Peak Heating in Shock Interference Regions at Hypersonic Speeds 1972 J. W. Keyes
D. J. Morris
1
+ Viscous and Inviscid Vortex Generation During Startup of Rocket Nozzles 1998 Francesco Nasuti
Marcello Onofri
1
+ Survey of viscous interactions associated with high Mach number flight 1971 Robert H. Korkegi
1