Laser Doppler velocity bias in separated turbulent flows

Addy Petrie , Samimy
Experiments in Fluids 6 ( 2) 80 -88

50
1988
Feedback control design for subsonic cavity flows

A. Serrani , Marco Debiasi , Marco Debiasi , J. Little
Applied and Computational Mathematics 8 ( 1) 70 -91

2
2009
Parallel fuel injection from the base of an extended strut into supersonic flow

J. M. Donbar , B. Sekar , J. F. Driscoll , T. H. Chen
American Institute of Aeronautics and Astronautics

11
1994
1990
Intermittent modal coupling in screeching underexpanded circular twin jets

J. Soria , M. Samimy , D. Edgington-Mitchell , G. Bell
Journal of Fluid Mechanics 910

2
2021
Effects of Nozzle Trailing Edges on Acoustic Field of Supersonic Rectangular Jet

C. W. Kerechanin , M. Samimy , J.-H. Kim
AIAA Journal 39 ( 6) 1065 -1070

55
2001
82
2002
Review of Planar Multiple-Component Velocimetry in High-Speed Flows

M. Samimy , M. P. Wernet
AIAA Journal 38 ( 4) 553 -574

97
2000
13
2000
Active Control of a Mach 0.9 Jet for Noise Mitigation Using Plasma Actuators

M. Samimy , J.-H. Kim , J. Kastner , I. Adamovich
AIAA Journal 45 ( 4) 890 -901

162
2007
Comparison of Noise Mechanisms in High and Low Reynolds Number High-Speed Jets

J. Kastner , M. Samimy , J. Hileman , J. B. Freund
AIAA Journal 44 ( 10) 2251 -2258

40
2006
Effect of plasma-based azimuthal mode excitation on supersonic jet flow

Datta Gaitonde , M. Samimy
5th Flow Control Conference

16
2010
11
2001
PROGRESS TOWARDS A REAL-TIME QUANTITATIVE MEASUREMENT TECHNIQUE FOR HIGH-SPEED FLOWS

B. Thurow , J. Hileman , M. Samimy , W. Lempert
15th AIAA Computational Fluid Dynamics Conference

7
2001
Logic-Based Active Control of Subsonic Cavity Flow Resonance

M. Debiasi , M. Samimy
AIAA Journal 42 ( 9) 1901 -1909

60
2004
Compressible separated flows

H. L. Petrie , M. Samimy , A. L. Addy
AIAA Journal 24 ( 12) 1971 -1978

35
1986
A study of compressible turbulent reattaching free shear layers

M. Samimy , H. L. Petrie , A. L. Addy
AIAA Journal 24 ( 2) 261 -267

79
1986
Structure of Supersonic Turbulent Boundary Layer After Expansion Regions

S. A. Arnette , M. Samimy , G. S. Elliott
AIAA Journal 33 ( 3) 430 -438

40
1995
Active Control of a High Reynolds Number Mach 0.9 Axisymmetric Jet

J.-H. Kim , J. Kastner , M. Samimy
AIAA Journal 47 ( 1) 116 -128

60
2009