Progress in Flight Physics
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Published By EDP Sciences

9782759806744, 9782759807178

Latest Documents Most Cited Documents Contributed Authors Related Sources Related Keywords

Reynolds number effect in a problem of sound generation by round and truncated cylinder streamlined by turbulent flow

Progress in Flight Physics ◽

10.1051/eucass/201203421 ◽

2012 ◽

Cited By ~ 1

Author(s):

V. Kopiev ◽

M. Zaitsev ◽

N. Ostrikov

Keyword(s):

Reynolds Number ◽

Turbulent Flow ◽

Sound Generation ◽

Reynolds Number Effect ◽

Truncated Cylinder

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Flow control in a supersonic inlet model by electrical discharge

Progress in Flight Physics ◽

10.1051/eucass/201203557 ◽

2012 ◽

Cited By ~ 7

Author(s):

S. Leonov ◽

D. Yarantsev ◽

F. Falempin

Keyword(s):

Flow Control ◽

Electrical Discharge ◽

Supersonic Inlet

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Experimental study and numerical modeling of vibrational oxygen temperature profiles behind a strong shock wave front

Progress in Flight Physics ◽

10.1051/eucass/201203231 ◽

2012 ◽

Cited By ~ 6

Author(s):

I. E. Zabelinskii ◽

L. B. Ibraguimova ◽

O. P. Shatalov ◽

Yu. V. Tunik

Keyword(s):

Shock Wave ◽

Experimental Study ◽

Numerical Modeling ◽

Wave Front ◽

Shock Wave Front ◽

Strong Shock ◽

Strong Shock Wave ◽

Temperature Profiles

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Development of a free round jet at different conditions at the nozzle exit under an acoustic action

Progress in Flight Physics ◽

10.1051/eucass/201203429 ◽

2012 ◽

Cited By ~ 3

Author(s):

Yu. A. Litvinenko ◽

G. R. Grek ◽

G. V. Kozlov ◽

A. M. Sorokin ◽

M. V. Litvinenko

Keyword(s):

Nozzle Exit ◽

Acoustic Action ◽

Round Jet

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Acoustic environment resulting in interaction of launch vehicle main engines jets with a launch pad having closed long ducts like a tunnel

Progress in Flight Physics ◽

10.1051/eucass/201203405 ◽

2012 ◽

Cited By ~ 2

Author(s):

V. V. Kudryavtsev ◽

A. V. Safronov

Keyword(s):

Launch Vehicle ◽

Acoustic Environment

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Global stability analysis - a key enabler in reduced order models and flow control

Progress in Flight Physics ◽

10.1051/eucass/201203491 ◽

2012 ◽

Author(s):

M. Morzyński ◽

W. Stankiewicz ◽

F. Thiele ◽

B. R. Noack ◽

G. Tadmor

Keyword(s):

Stability Analysis ◽

Flow Control ◽

Global Stability ◽

Reduced Order Models ◽

Reduced Order ◽

Global Stability Analysis

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Flow structure and turbulence in near fields of circular and noncircular jets

Progress in Flight Physics ◽

10.1051/eucass/201203041 ◽

2012 ◽

Cited By ~ 1

Author(s):

N. E. Öçer ◽

G. Taşar ◽

O. Uzol ◽

S. Özgen

Keyword(s):

Flow Structure ◽

Circular And Noncircular Jets

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Model reduction and control of a separating boundary-layer flow

Progress in Flight Physics ◽

10.1051/eucass/201203471 ◽

2012 ◽

Author(s):

U. Ehrenstein ◽

P.-Y. Passaggia ◽

F. Gallaire

Keyword(s):

Boundary Layer ◽

Model Reduction ◽

Boundary Layer Flow ◽

Layer Flow ◽

And Control

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Aircraft dynamic lateral stability analytic formulation for dutch roll mode stability prediction

Progress in Flight Physics ◽

10.1051/eucass/201203053 ◽

2012 ◽

Cited By ~ 2

Author(s):

M. J. Bazile ◽

M. F. Calderara

Keyword(s):

Lateral Stability ◽

Stability Prediction ◽

Mode Stability ◽

Dutch Roll

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Simulation of oxygen atom heterogeneous recombination on Al2O3fromab initioapproach

Progress in Flight Physics ◽

10.1051/eucass/201203351 ◽

2012 ◽

Cited By ~ 2

Author(s):

V. L. Kovalev ◽

A. A. Kroupnov ◽

M. Ju. Pogosbekian ◽

L. P. Sukhanov

Keyword(s):

Oxygen Atom ◽

Heterogeneous Recombination

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Progress in Flight PhysicsLatest Publications

TOTAL DOCUMENTS

H-INDEX

Published By EDP Sciences

Reynolds number effect in a problem of sound generation by round and truncated cylinder streamlined by turbulent flow

Flow control in a supersonic inlet model by electrical discharge

Experimental study and numerical modeling of vibrational oxygen temperature profiles behind a strong shock wave front

Development of a free round jet at different conditions at the nozzle exit under an acoustic action

Acoustic environment resulting in interaction of launch vehicle main engines jets with a launch pad having closed long ducts like a tunnel

Global stability analysis - a key enabler in reduced order models and flow control

Flow structure and turbulence in near fields of circular and noncircular jets

Model reduction and control of a separating boundary-layer flow

Aircraft dynamic lateral stability analytic formulation for dutch roll mode stability prediction

Simulation of oxygen atom heterogeneous recombination on Al2O3fromab initioapproach

Progress in Flight Physics
Latest Publications