Jeffrey Kastner

Jeffrey Kastner

Associate Professor Educator

Edwards Center

4150A EDWARDS 1

CEAS - Engineering & Computing Education -

Research Support

Grant: #P0400014253 Investigators:Gutmark, Ephraim; Kastner, Jeffrey 04-15-2009 -03-30-2010 General Electric Global Research Experimental and Computational Investigation of the Effects of Vortex Generators on Deflagration-to-Detonation Transition Length Role:PI $20,000.00 Closed Level:Industry

Grant: #PO 200-1J-14E43390 Investigators:Gutmark, Ephraim; Kastner, Jeffrey 05-26-2009 -12-31-2010 General Electric Aviation F101 Rig Test Role:PI $75,033.00 Closed Level:Industry

Grant: #CK# 3025 Investigators:Gutmark, Ephraim; Kastner, Jeffrey 08-23-2008 -12-31-2009 Department of the Navy Innovative Aircraft Engine Noise Reduction using Tailored and Smart Acoustic Liners Role:PI $21,500.00 Closed Level:Federal

Grant: #PO 200-1J-14E44425 Investigators:Gutmark, Ephraim; Kastner, Jeffrey 07-01-2009 -12-31-2009 General Electric Aviation Combustion Testing Role:Collaborator $130,317.00 Closed Level:Industry

Grant: #N00173-10-1-G-018 Investigators:Gutmark, Ephraim; Kastner, Jeffrey 06-25-2010 -06-24-2013 Department of the Navy Fundamental Jet Noise Reduction Science and Technology- Validation Experiments Role:Collaborator $510,000.00 Active Level:Federal

Grant: #SB1107-001-1 / NNX11CG68P Investigators:Gutmark, Ephraim; Kastner, Jeffrey 02-01-2011 -08-01-2011 National Aeronautics and Space Administration Development of Wavelet Stochastic Estimation for Identifying the Contribution of Turbulent Structures to the Sound Field of Shear Flows Role:PI $30,500.00 Closed Level:Federal

Grant: #PO 200-18-14A32044 Investigators:Gutmark, Ephraim; Kastner, Jeffrey 01-01-2011 -12-31-2011 General Electric Aviation Jet Noise Reduction (USA Program) Role:Collaborator $145,000.00 Closed Level:Industry

Grant: #SB1113-001-1 \ N68335-11-C-0462 Investigators:Gutmark, Ephraim; Kastner, Jeffrey 08-25-2011 -08-16-2012 Department of the Navy Gas Turbine Engine Exhaust Jet Shear-Layer Pressure Measurement System Role:PI $25,000.00 Closed Level:Federal

Grant: #Subcontract 21 \ FA8650-11-C-2191 Investigators:Gutmark, Ephraim; Kastner, Jeffrey 08-22-2011 -01-31-2012 Department of the Air Force Ignition Testing on an F101 Pilot Can Role:Collaborator $75,000.00 Active Level:Federal

Grant: #200-1J-14016236 Investigators:Gutmark, Ephraim; Kastner, Jeffrey 05-01-2012 -04-30-2013 General Electric Aviation Combustion Testing AFJ Role:Collaborator $160,000.00 Active Level:Industry

Grant: #1096.JN.12.01 \ FA8650-08-C-2851 Investigators:Gutmark, Ephraim; Kastner, Jeffrey 06-25-2012 -09-14-2013 Department of the Air Force Wall-Mounted Thermally Stable Catalysts for Augmentor Flame Stabilization. Task 5 Role:Collaborator $54,998.00 Active Level:Federal

Grant: #PO 200-1J-14Q16258 Investigators:Gutmark, Ephraim; Kastner, Jeffrey; Munday, David 07-01-2012 -12-31-2013 General Electric Aviation Turbine Airfoil Cascade Test Role:Collaborator $233,652.00 Active Level:Industry

Grant: #Engineering Models I and II Investigators:Boerio, F James; Bucks, Gregory; Kastner, Jeffrey; Ossman, Kathleen; Roseman, Rodney; Torsella, Joni 03-11-2013 -03-10-2014 MathWorks, Inc. Inclusion of Data Acquisition Technology in a Collection of Introductory Engineering Courses Role:Collaborator $37,131.00 Active Level:Industry

Grant: #EEC-1404766 Investigators:Angelopoulos, Anastasios; Bhattacharya, Prabir; Cohen, Kelly; Franco, John; Guliants, Vadim; Kastner, Jeffrey; Kukreti, Anant; Kupferle, Margaret; Lu, Mingming; Nistor, Vasille; Sorial, George; Wei, Heng; Wendell, David 05-01-2014 -04-30-2017 National Science Foundation RET Site on "Challenge-Based Learning and Engineering Design Process Enhanced Research Experiences for Middle and High School In-Service Teachers." Role:Collaborator $498,949.00 Awarded Level:Federal

Grant: #DUE-2337003 Investigators:Bucks, Gregory; Kastner, Jeffrey; Murphy, TJ; Reeping, David; Sorby, Sheryl 04-15-2024 -03-31-2027 National Science Foundation Expanding Pathways for Preparing the Next Generation of Engineers: First-Year Engineering 2.0 (FYE2.0) Role:Collaborator 719915.00 Active Level:Federal

Publications

Peer Reviewed Publications

Mora P.;Kastner J.;Gutmark E.J.;Kailasanath K. (01-01-2015. ) Investigation of a heated supersonic jet chevrons nozzle.53rd AIAA Aerospace Sciences Meeting, , More Information

Mora P.;Heeb N.;Kastner J.;Gutmark E.J.;Kailasanath K. (01-01-2014. ) Impact of heat on the pressure skewness and kurtosis in supersonic jets.AIAA Journal, , 52 (4 ) ,777-787 More Information

Mora P.;Heeb N.;Kastner J.;Gutmark E.J.;Kailasanath K. (12-17-2013. ) Near-and far-field pressure skewness and kurtosis in heated supersonic jets from round and chevron n.Proceedings of the ASME Turbo Expo, , 2 , More Information

Heeb N.;Kastner J.;Gutmark E.;Kailasanath K. (12-01-2013. ) Supersonic jet noise reduction by chevrons and fluidic injection.International Journal of Aeroacoustics, , 12 (7-8 ) ,679-698 More Information

Mora P.;Heeb N.;Kastner J.;Gutmark E.J.;Kailasanath K. (08-19-2013. ) Effect of scale on the far-field pressure skewness and kurtosis of heated supersonic jets .51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013, ,

Mihescu M.;Kastner J.;Gutmark E. (12-01-2012. ) Tertiary flow effects on a co-axial ducted jet .50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, ,

Kastner J.;Heeb N.;Gutmark E.;Liu J.;Kailasanath K. (12-01-2012. ) Using chevrons and fluidic injection to reduce supersonic jet noise .41st International Congress and Exposition on Noise Control Engineering 2012, INTER-NOISE 2012, , 5 ,4291-4301

Kastner J.;Malla B.;Gutmark E.;Liu J.;Kailasanath K. (12-01-2012. ) Using wavelet stochastic estimation to correlate near-field pressure to velocity pod modes in a supe .50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, ,

Gutmark E.; Heeb N.; Kailasanath K.; Kastner J.; Liu J.; Mora P. (12-01-2012. ) Mode switching of jet noise screech .18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference), ,

Liu J.;Kailasanath K.;Ramammurti R.;Heeb N.;Kastner J.;Gutmark E. (12-01-2012. ) Numerical investigation of fluidic enhanced chevrons for noise reduction in supersonic jets .50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, ,

Mora P.;Kastner J.;Heeb N.;Munday D.;Gutmark E.;Liu J.;Kailasanath K. (12-01-2012. ) The impact of heat on the near and far-field pressure skewness in supersonic jets.50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, , More Information

Suresh S.;Lim T.C.;Kastner J. (07-01-2012. ) Predicting acoustic transmission loss through laminated glass with air and porous layers.International Journal of Vehicle Noise and Vibration, , 8 (3 ) ,237-260 More Information

Malla B.;Mihaescu M.;Kastner J.;Gutmark E. (06-20-2012. ) Proper orthogonal decomposition on LES and PIV data sets from a mach 0.9 jet .50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, ,

Kastner J.; Lim T.; Suresh S. (12-01-2011. ) Transmission loss analysis through porous laminated glass using transfer matrices.SAE Technical Papers, , More Information

Pendleton S.;Kastner J.;Gutmark E.;Gundersen M. (11-01-2011. ) Surface streamer discharge for plasma flow control using nanosecond pulsed power.IEEE Transactions on Plasma Science, , 39 (11 PART 1 ) ,2072-2073 More Information

Rask O.;Kastner J.;Gutmark E. (08-01-2011. ) Understanding how chevrons modify noise in a supersonic jet with flight effects.AIAA Journal, , 49 (8 ) ,1569-1576 More Information

Kastner J.;Cuppoletti D.;Malla B.;Gutmark E. (12-13-2010. ) Optimization of stochastic estimation techniques in a high-speed, Axisymmetric jet .48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, ,

Perrino M.;Kastner J.;Gutmark E.;Gogineni S. (12-13-2010. ) Towards development of an active single-layer acoustic liner for jet engine noise reduction .48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, ,

Cuppoletti D.;Kastner J.;Gutmark E. (12-02-2010. ) Stochastic Estimation of velocity using near-field pressure in a coaxial jet with chevrons .40th AIAA Fluid Dynamics Conference, ,

Mignee J.;Kastner J.;Munday D.;Heeb N.;Gutmark E.;Liu J.;Kailasanath K. (12-02-2010. ) Proper Orthogonal Decomposition analysis of numerically simulated supersonic jet flow .40th AIAA Fluid Dynamics Conference, ,

Reed J.;Cuppoletti D.;Kastner J.;Gutmark E. (12-01-2009. ) Experimental analysis of screech tone effects for a V-Gutter stabilized flame .47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, ,

Kastner J.;Harris C.;Mignee J.;Gutmark E. (12-01-2009. ) Linear stochastic estimation of the flowfield from a Bypass Ratio 8 nozzle configuration .47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, ,

Cuppoletti D.;Kastner J.;Reed J.;Gutmark E. (12-01-2009. ) High frequency combustion instabilities with radial V-gutter flameholders .47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, ,

Kastner J.;Cuppoletti D.;Gutmark E.;Fahrland A.;Jeffries J.;Hanson R. (12-01-2009. ) Simultaneous measurement of flow fluctuations and near-field pressure in a subsonic jet .15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference), ,

Kim J.;Kastner J.;Samimy M. (01-01-2009. ) Active control of a high reynolds number Mach 0.9 axisymmetric Jet.AIAA Journal, , 47 (1 ) ,116-128 More Information

Kastner J.;Kim J.H.;Samimy M. (12-01-2008. ) Toward better understanding of far-field radiated noise mechanisms in a high Reynolds number Mach 0. 46th AIAA Aerospace Sciences Meeting and Exhibit, ,

Samimy M.;Kim J.H.;Kastner J.;Adamovich I. (12-01-2007. ) Noise mitigation in high speed and high reynolds number jets using plasma actuators .13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference), ,

Kastner J.;Kim J.H.;Samimy M. (07-03-2007. ) Correlation of large-scale structure dynamics and far-field radiated noise in a mach 0.9 jet .Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting, , 15 ,10062-10078

Kim J.H.;Kastner J.;Adamovich I.;Samimy M. (07-03-2007. ) Active control of high subsonic jets .Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting, , 6 ,3900-3914

Utkin Y.G.;Keshav S.;Kim J.H.;Kastner J.;Adamovich I.V.;Samimy M. (07-02-2007. ) Characterization of localized arc filament plasma actuators used for high-speed flow control .Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting, , 14 ,9644-9664

Samimy M.;Kim J.H.;Kastner J.;Adamovich I.;Utkin Y. (05-10-2007. ) Active control of high-speed and high-Reynolds-number jets using plasma actuators.Journal of Fluid Mechanics, , 578 ,305-330 More Information

Samimy M.;Kim J.H.;Kastner J.;Adamovich I.;Utkin Y. (04-01-2007. ) Active control of a Mach 0.9 jet for noise mitigation using plasma actuators.AIAA Journal, , 45 (4 ) ,890-901 More Information

Utkin Y.G.;Keshav S.;Kim J.H.;Kastner J.;Adamovich I.V.;Samimy M. (02-07-2007. ) Development and use of localized arc filament plasma actuators for high-speed flow control.Journal of Physics D: Applied Physics, , 40 (3 ) ,685-694 More Information

Kastner J.;Kim J.H.;Samimy M. (12-27-2006. ) Noise sources in controlled high reynolds number and high speed jets .Collection of Technical Papers - 12th AIAA/CEAS Aeroacoustics Conference, , 5 ,3278-3290

Samimy M.;Kim J.H.;Adamovich I.;Utkin Y.;Kastner J. (12-27-2006. ) Toward noise mitigation in high speed and high reynolds number jets using plasma actuators .Collection of Technical Papers - 12th AIAA/CEAS Aeroacoustics Conference, , 6 ,3885-3901

Samimy M.;Kastner J.;Kim J.H.;Utkin Y.;Adamovich I.;Brown C. (12-11-2006. ) Flow and noise control in high speed and high Reynolds number jets using plasma actuators .Collection of Technical Papers - 3rd AIAA Flow Control Conference, , 1 ,76-91

Samimy M.;Kim J.H.;Adamovich I.;Utkin Y.;Kastner J. (12-01-2006. ) Active control of high speed and high reynolds number free jets using plasma actuators .Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting, , 12 ,8533-8549

Kastner J.;Samimy M.;Hileman J.;Freund J.B. (10-01-2006. ) Comparison of noise mechanisms in high and low reynolds number high-speed jets.AIAA Journal, , 44 (10 ) ,2251-2258 More Information

Kastner J.;Samimy M.;Hileman J.;Freund J.B. (12-29-2005. ) Comparison of noise sources in high and low reynolds number high speed jets .Collection of Technical Papers - 11th AIAA/CEAS Aeroacoustics Conference, , 5 ,3628-3639

Trolinger J.;L'Esperance D.;Kim J.;Kastner J.;Lempert W.;Samimy M. (12-01-2005. ) Optical diagnostics for quantifying flow control effects on aero optical wavefront degradation .36th AIAA Plasmadynamics and Lasers Conference, ,

Samimy M.;Adamovich I.;Webb B.;Kastner J.;Hileman J.;Keshav S.;Palm P. (10-01-2004. ) Development and characterization of plasma actuators for high-speed jet control.Experiments in Fluids, , 37 (4 ) ,577-588 More Information

Kastner J.;Hileman J.;Samimy M. (07-01-2004. ) Exploring high-speed axisymmetric jet noise control using Hartmann tube fluidic actuators .AIAA Paper, , 1997-2009

Samimy M.;Adamovich I.;Webb B.;Kastner J.;Hileman J.;Keshav S.;Palm P. (07-01-2004. ) Developement and application of localized arc filament plasma actuators for jet flow and noise contr .AIAA Paper, , 1976-1985

Kastner J.;Samimy M. (12-01-2003. ) Effects of forcing frequency on the control of an impinging high-speed jet .41st Aerospace Sciences Meeting and Exhibit, ,

Kastner J.;Samimy M. (12-01-2002. ) Development and characterization of Hartmann tube based fluidic actuators for high speed flow contro .40th AIAA Aerospace Sciences Meeting and Exhibit, ,

Samimy M.;Kastner J.;Debiasi M. (12-01-2002. ) Control of high-speed impinging jets using hartmann tube fluidic actuators .1st Flow Control Conference, ,

Kastner J.;Samimy M. (01-01-2002. ) Development and characterization of Hartmann tube fluidic actuators for high-speed flow control.AIAA Journal, , 40 (10 ) ,1926-1934 More Information