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Progress in Flight Physics
Latest Publications
TOTAL DOCUMENTS
37
(FIVE YEARS 0)
H-INDEX
6
(FIVE YEARS 0)
Published By EDP Sciences
9782759808779, 9782759810420
Latest Documents
Most Cited Documents
Contributed Authors
Related Sources
Related Keywords
Latest Documents
Most Cited Documents
Contributed Authors
Related Sources
Related Keywords
Numerical analysis of three complex three-dimensional shock wave / turbulent boundary layer interaction flows
Progress in Flight Physics
◽
10.1051/eucass/201305247
◽
2013
◽
Cited By ~ 2
Author(s):
A. D. Grosvenor
◽
A. A. Zheltovodov
◽
M. A. Matheson
◽
L. M. Sailer
◽
M. Krzysztopik
◽
...
Keyword(s):
Boundary Layer
◽
Shock Wave
◽
Numerical Analysis
◽
Turbulent Boundary Layer
◽
Three Dimensional
◽
Layer Interaction
◽
Boundary Layer Interaction
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Direct numerical simulations of mack-mode damping on porous coated cones
Progress in Flight Physics
◽
10.1051/eucass/201305057
◽
2013
◽
Author(s):
H. Lüdeke
◽
V. Wartemann
Keyword(s):
Numerical Simulations
◽
Direct Numerical Simulations
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Delta wing with blunted leading edges at angle of attack in hypersonic flow
Progress in Flight Physics
◽
10.1051/eucass/201305415
◽
2013
◽
Author(s):
P. Vashchenkov
◽
A. Kashkovsky
◽
M. Ivanov
Keyword(s):
Hypersonic Flow
◽
Delta Wing
◽
Angle Of Attack
◽
Leading Edges
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Evaluation of the aerodynamic properties of the intermediate experimental vehicle in the rarefied and transitional regime
Progress in Flight Physics
◽
10.1051/eucass/201305425
◽
2013
◽
Cited By ~ 1
Author(s):
T. Bányai
◽
E. Torres
◽
T. E. Magin
◽
A. V. Kashkovsky
◽
P. V. Vashchenkov
◽
...
Keyword(s):
Transitional Regime
◽
Aerodynamic Properties
◽
Experimental Vehicle
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Base-flow sensitivity of a generic rocket forebody towards small freestream angles
Progress in Flight Physics
◽
10.1051/eucass/201305169
◽
2013
◽
Cited By ~ 2
Author(s):
C. C. Wolf
◽
Y. You
◽
R. Hörnschemeyer
◽
H. Lüdeke
◽
V. Hannemann
Keyword(s):
Base Flow
◽
Flow Sensitivity
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Modeling Intermediate eXperimental Vehicle control thruster plume-surface interaction
Progress in Flight Physics
◽
10.1051/eucass/201305545
◽
2013
◽
Author(s):
A. V. Kashkovsky
◽
P. V. Vashchenkov
◽
T. Bányai
◽
M. S. Ivanov
Keyword(s):
Vehicle Control
◽
Surface Interaction
◽
Experimental Vehicle
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Flowfields around supersonic aerodynamic bodies under the action of asymmetric energy release
Progress in Flight Physics
◽
10.1051/eucass/201305139
◽
2013
◽
Cited By ~ 3
Author(s):
O. A. Azarova
◽
D. Knight
◽
Yu. F. Kolesnichenko
Keyword(s):
Energy Release
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Transport properties of partially ionized atomic gases with electronic excitation
Progress in Flight Physics
◽
10.1051/eucass/201305533
◽
2013
◽
Author(s):
V. A. Istomin
◽
E. V. Kustova
Keyword(s):
Transport Properties
◽
Electronic Excitation
◽
Atomic Gases
◽
Partially Ionized
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Stability of symmetric vortex flow over slender bodies and possibility of control by local gas heating
Progress in Flight Physics
◽
10.1051/eucass/201305155
◽
2013
◽
Cited By ~ 2
Author(s):
V. I. Shalaev
◽
I. V. Shalaev
Keyword(s):
Vortex Flow
◽
Gas Heating
◽
Slender Bodies
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Supersonic laminar separated flow structure at a ramp for a free-stream mach number of 6
Progress in Flight Physics
◽
10.1051/eucass/201305349
◽
2013
◽
Cited By ~ 6
Author(s):
V. I. Zapryagaev
◽
I. N. Kavun
◽
I. I. Lipatov
Keyword(s):
Mach Number
◽
Flow Structure
◽
Free Stream
◽
Separated Flow
◽
Free Stream Mach Number
◽
Supersonic Laminar
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