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Publications, proceedings, abstracts, oral presentations, and other media (PDF) from 2001 - present

Detailed listing of GDL's published articles and conference proceedings from 2006 to present

2023 | 2022 | 2021 | 2020 | 2019 | 2018 | 2017 | 2016 | 2015 | 2014 | 2013 | 2012 | 2011| 2010 | 2009 | 2008 | 2007 | 2006

2023 (6) up arrow to top of list

  • Willis, W.A., Valdez, J.A., Tinney, C.E., Hamilton, M.F., A machine learning approach to identifying waveform coalescence in supersonic jet noise. AIAA Aviation 2023 Forum, AIAA Paper 2023-3353 (2023). San Diego, California, USA. 10.2514/6.2023-3353
  • Tinney, C.E., Valdez, J.A., Zhao-Dubuc, Y., A moving source model for rotor broadband noise. AIAA Aviation 2023 Forum, AIAA Paper 2023-3222 (2023). San Diego, California, USA. 10.2514/6.2023-3222
  • Willis, W.A., Valdez, J.A., Pineau, P., Bogey, C., Tinney, C.E., Hamilton, M.F., A study of Mach wave coalescence using spark sources and large-eddy simulation. AIAA Scitech 2023 Forum, AIAA Paper 2023-0021 (2023). National Harbor, Maryland, USA. 10.2514/6.2023-0021
  • Tinney, C.E., Zhao-Dubuc, Y., POD-based reduced-order models in translating coordinates. AIAA Scitech 2023 Forum, AIAA Paper 2023-1986 (2023). National Harbor, Maryland, USA. 10.2514/6.2023-1986
  • Tinney, C.E., Valdez, J.A., Higher-order statistical metrics for characterizing rotor acoustics. AIAA Scitech 2023 Forum, AIAA Paper 2023-1350 (2023). National Harbor, Maryland, USA. 10.2514/6.2023-1350
  • Tinney, C.E., The effect of nozzle contour on the vibroacoustic loads that form from high area ratio nozzles during sea level launch. The 184th Meeting of the Acoustical Society of America. 153, 3 Pt. 2 of 2 (2023). Chicago, Illinois, USA.

2022 (3) up arrow to top of list

  • Valdez, J. A., Tinney, C. E., Wake of a coaxial corotating rotor in hover. AIAA Journal. 10.2514/1.J061651
  • Valdez, J. A., Tinney, C. E., The unsteady wake produced by a coaxial co-rotating rotor in hover. AIAA Scitech 2022 Forum, AIAA Paper 2022-2166 (2022). San Diego, California, USA. 10.2514/6.2022-2166
  • Willis, W. A., Tinney, C. E., Hamilton, M. F., Cormack, J. M., Reduced-order models of coalescing Mach waves. AIAA Scitech 2022 Forum, AIAA Paper 2022-1792 (2022). San Diego, California, USA. 10.2514/6.2022-1792

2021 (4) up arrow to top of list

  • Willis, W. A., Cormack, J., Tinney, C. E., Hamilton, M. F. Examination of Mach wave coalescence in a Mach 3 jet flow. The 181st Meeting of the Acoustical Society of America. 150, 4 Pt. 2 of 2 (2021). Seattle, Washington, USA. 10.1121/10.0008034. Invited.
  • Baars, W. J., Murray, N. E., Tinney, C. E. A proper framework for studying noise from jets with non-compact sources. Journal of Fluid Mechanics (pp. 1-32). 929, A23 (2021). 10.1017/jfm.2021.837
  • Tinney, C. E., Valdez, J., Murray, N. Supersonic jets with compliant wall nozzles. AIAA Scitech 2021 Forum, Virtual, AIAA Paper 2021–1524 (2021). Virtual. 10.2514/6.2021-1524. Winner of the 2021 AIAA/CEAS Aeroacoustics Best Paper Award.
  • Tinney, C. E. Sparse Biorthogonal Decomposition. AIAA Scitech 2021 Forum, Virtual, AIAA Paper 2021–1851 (2021). 10.2514/6.2021-1851

2020 (3) up arrow to top of list

  • Martelli, E., Saccoccio, L., Ciottoli, P. P., Tinney, C. E., Baars, W. J., Bernardini, M. Flow dynamics and wall-pressure signatures in a high-Reynolds number overexpanded nozzle with free shock separation. Journal of Fluid Mechanics (pp. 1-30). 895, A29 (2020). 10.1017/jfm.2020.280
  • Tinney, C. E., Valdez, J. A., Murray, N. Aerodynamic performance of augmented supersonic nozzles. Experiments in Fluids. 61, 48 (2020). 10.1007/s00348-019-2866-3
  • Tinney, C. E., Valdez, J. A. Thrust and acoustic performance of small-scale, coaxial, co-rotating rotors in hover. AIAA Journal (pp 1657-1667). 58, 4 (2020). 10.2514/1.J058489

2019 (7) up arrow to top of list

  • Hay, T.A., Valdez, J. A., Tinney, C. E., Hamilton, M. F., Schram, C. Sampling Artifacts in Quantitative Schlieren. 25th AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2019-2635 (2019). Delft, The Netherlands. 10.2514/6.2019-2635
  • Tinney, C. E., Valdez, J. A., Meier, H., Ruf, J. Laboratory Scale Testing of Ignition Overpressure for Space Vehicle Launch Pad Environments. 25th AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2019-2413 (2019). Delft, The Netherlands. 10.2514/6.2019-2413
  • Tinney, C. E., Schram, C. Acoustic Modes from a Mach 3 Jet. 25th AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2019-2598 (2019). Delft, The Netherlands. 10.2514/6.2019-2598
  • Tinney, C. E., Valdez, J. Acoustic scaling for small rotors in hover. 2019 American Helicopter Society 75th Annual Forum (2019). Philadelphia, Pennsylvania USA. Link to paper
  • Eitner, M. A., Miller, B. G., Sirohi, J., Tinney, C. E. Operational Modal Analysis of a Thin-Walled Rocket Nozzle using Phase-Based Image Processing and Complexity Pursuit. IMAC-XXXVII Conference & Exposition on Structural Dynamics (pp 1-17) (2019). Orlando, Florida USA. 10.1007/978-3-030-12935-4_3. Winner of the Best Paper Award in Optical Techniques & Computer Vision.
  • Eitner, M., Sirohi, J., Tinney, C. E. Modal parameter estimation of a reduced-scale rocket nozzle using blind source separation. Measurement Science Technology Journal (pp 1-13) 30 (2019). 10.1088/1361-6501/ab228f
  • Tinney, C. E., Shipman, L,., Panickar, P. Proper-orthogonal-decomposition-based reduced-order models for characterizing ship airwake interactions. AIAA Journal (pp 633-646) 58, 2 (2019). 10.2514/1.J058499

2018 (5) up arrow to top of list

  • Tinney, C. E., Panickar, P., Vogel, P. Aeroacoustics of a Planar Multistream Supersonic Nozzle with Aft Deck and Sidewalls. AIAA Journal (pp 3926–3937) 56, 10 (2018). 10.2514/1.J056735
  • Valdez, J. A., Tinney, C E. Measurements of a Mach 3 jet using high-speed optical flow techniques. AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2018-3148 (2018). Atlanta, Georgia USA. 10.2514/6.2018-3148
  • Tinney, C. E., Sirohi, J. Multirotor Drone Noise at Static Thrust. AIAA Journal (pp 2816-2826) 56, 7 (2018). 10.2514/1.J056827
  • Tinney, C E., Valdez, J. A. A new test stand for measuring wall shear stress. AIAA Fluid Dynamics Conference, AIAA Paper 2018-3085 (2018). Atlanta, Georgia USA. 10.2514/6.2018-3085
  • Tinney, C. E., Shipman, J., Panickar, P. Reduced-Order Models for Characterizing Ship Airwake Interactions. AAIAA Fluid Dynamics Conference, AIAA Paper 2018-3233 (pp 1-17) (2018). Atlanta, Georgia USA. 10.2514/6.2018-3233

2017 (5) up arrow to top of list

  • Stephenson, J. H., Tinney, C. E. Extracting Blade-Vortex Interactions Using Continuous Wavelet Transforms. Journal of the American Helicopter Society (pp 1-10) 62 (2017). 10.4050/JAHS.62.022001
  • Tinney, C. E., Hill, B., Valdez, and J. A., Sirohi, J., Cameron, C. Drone acoustics at static thrust conditions. American Helicopter Society 73rd Annual Forum, (2017). Fort Worth, Texas USA. Link to paper
  • Tinney, C. E., Scott, K., Routon, M., Sirohi, J., Ruf, J. H. Effect of aeroelasticity on vibroacoustic loads during startup of large area ratio nozzles. 23rd AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2017-3361 (2017). Denver, Colorado USA. 10.2514/6.2017-3361
  • Joseph, J., Tinney, C. E., Murray, N. Ideal gas effects in aeroacoustics. 55th AIAA Aerospace Sciences Meeting, AIAA Paper 2017-0688 (2017). Grapevine, Texas USA. 10.2514/6.2017-0688
  • Tinney, C. E. Wall pressure unsteadiness on the aft deck of a planar multi-stream supersonic nozzle. 55th AIAA Aerospace Sciences Meeting, AIAA Paper 2017-0525 (2017). Grapevine, Texas USA. 10.2514/6.2017-0525

2016 (8) up arrow to top of list

  • Canchero, A., Tinney, C. E., Murray, N., Ruf, J. H. Acoustic imaging of clustered rocket nozzles undergoing end-effects. AIAA Journal (pp 3778-3786) 54, 12 (2016). 10.2514/1.J055053
  • Rojo, R., Tinney, C E., Ruf, J. H. Effect of stagger on the vibroacoustic loads from clustered rockets. AIAA Journal (pp 3588-3597) 54, 11 (2016). 10.2514/1.J055017
  • Baars, W. J., Tinney, C. E., Hamilton, M. F. A piecewise spreading regime model for calculating effective Gol'dberg numbers for supersonic jet noise. AIAA Journal (pp 2833-2842) 54, 9 (2016). 10.2514/1.J054790
  • Canchero, A., Tinney, C. E., N. Murray, N., Ruf, J. H. Flow and acoustics of clustered rockets during startup. AIAA Journal (pp 1660-1669) 54, 5 (2016). 10.2514/1.J054622
  • R. Fievet, R., Tinney, C. E., Baars, W. J., Hamilton, M. F. Coalescence in the sound field of a laboratory-scale supersonic jet. AIAA Journal (pp 254-265) 54, 1 (2016). 10.2514/1.J054252
  • Joseph, J., Tinney, C. E. A combustion model for studying the effect of ideal gas properties on jet noise Bulletin of the American Physical Society 61, 20 (2016). Portland, Oregon USA, Link to abstract
  • Rojo, R., Tinney, C. E., Ruf, J. H. Effect of stagger on the vibroacoustic loads from clustered rockets. 54th AIAA Aerospace Sciences Meeting, AIAA Paper 2016-1016 (2016). San Diego, California USA. 10.2514/1.J055017
  • Valdez, J. A., Tinney, C. E. A new thrust stand for testing multi-stream and heat simulated supersonic nozzles. 54th AIAA Aerospace Sciences Meeting, AIAA Paper 2016-1890 (2016). San Diego, California USA. 10.2514/6.2016-1890

2015 (5) up arrow to top of list

  • Baars, W. J., Tinney, C. E., Ruf, J. H. Non-stationary shock motion unsteadiness in an axisymmetric geometry with pressure gradient. Experiments in Fluids (pp 1-18) 56, 92 (2015) 10.1007/s00348-015-1958-y
  • Mula, S. M., Tinney, C. E. A study of the turbulence within a spiraling vortex filament using proper orthogonal decomposition. Journal of Fluid Mechanics (pp 570-589) 769 (2015) 10.1017/jfm.2015.104
  • Canchero, A., Rojo, R., Tinney, C. E., Murray, N., Ruf, J. H. (2015) Shadowgraphy of the end-effects regime produced by clustered rockets. Proceedings of the 15th European Turbulence Conference, Delft, The Netherlands. Online proceedings at: https://www.researchgate.net/publication/291973620_SHADOWGRAPHY_OF_THE_END-EFFECTS_REGIME_PRODUCED_BY_CLUSTERED_ROCKETS
  • Mack, G., Tinney, C. E., Ruf, J. H. Reliable methods for predicting the sound from clustered rocket engines. Proceedings of the 15th European Turbulence Conference, Delft, The Netherlands. 1 Online proceedings at: https://repository.tudelft.nl/islandora/object/uuid%3A4dcd7f79-2ec0-4112-b00d-8b21d1e56361
  • Tinney, C. E., Canchero, A., Rojo, R., Mack, G., Murray, N. E. Ruf, J. H. The sound-field produced by clustered rockets during start-up. Whither Turbulence and Big Data for the 21st Century. Symposium held at the Institute d'Etudes Scientifiques de Cargese, Corsica, France, (2015) Published with Springer Hardbound Volumes. 10.1007/978-3-319-41217-7

2014 (11) up arrow to top of list

  • Baars, W. J., Tinney, C. E. Proper orthogonal decomposition-based Spectral Higher-order Stochastic Estimation. Physics of Fluids (pp 1-20) 26, 055112 (2014) 10.1063/1.4879255
  • Stephenson, J. H., Tinney, C. E., Watts, M. E., Greenwood, E., Time frequency analysis of sound from a maneuvering rotorcraft. Journal of Sound and Vibration (pp 5324-5339) 333, 21 (2014)
  • Baars, W. J., Tinney, C. E. Shock-structures in the acoustic field of a Mach 3 jet with crackle. Journal of Sound and Vibration (pp 2539-2553) 333, 12 (2014)
  • Baars, W. J., Tinney, C. E., Wochner, M. S., Hamilton, M. On cumulative nonlinear acoustic waveform distortions from high-speed jets. Journal of Fluid Mechanics (pp 331-366) 749 (2014) 10.1017/jfm.2014.228
  • Karpatne, A., Sirohi, J., Mula, S., Tinney, C .E. Vortex ring model of tip vortex aperiodicity in a hovering helicopter rotor. Journal of Fluids Engineering (pp 1-9) 136, 7, 071104 (2014)
  • Donald, B. W., Baars, W. J., Tinney, C. E., Ruf, J. H.Sound produced by large area ratio rocket nozzles during fixed and transient operations. AIAA Journal (pp 1474-1485) 52, 7, 10.2514/1.J052588
  • Baars, W. J., Tinney, C. E., Hamilton, M. F.} Challenges associated with studying nonlinear distortion of acoustic waveforms emitted by high-speed jets. 43rd International Congress on Noise Control Engineering, Australian Acoustical Society, Melbourne, Australia.
  • Fi'evet, R., Tinney, C. E., Baars, W. J., Hamilton, M. F. Acoustic waveforms produced by a laboratory scale supersonic jet. 20th AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2014-2906 (2014). Atlanta, Georgia, USA.
  • Mula, S. M., Tinney, C. E. Classical and snapshot forms of the POD techniques applied to a helical vortex filament. 44th AIAA Fluid Dynamics Conference, AIAA Paper 2014-3257 (2014). Atlanta, Georgia, USA.
  • Stephenson, J. H., Tinney, C. E. Extracting blade vortex interactions using continuos wavelet transforms. American Helicopter Society 70th Annual Forum. (2017). Montreal, Canada.
  • Mula, S. M., Cameron, C,. Tinney, C. E., Sirohi, J. Low-dimensional characteristics of tip vortices from a coaxial rotor in hover American Helicopter Society 70th Annual Forum. (2017). Montreal, Canada.

2013 (7) up arrow to top of list

  • Mula, S. M., Stephenson, J. H., Tinney, C. E., Sirohi, J. Dynamical characteristics of the tip vortex from a four-bladed rotor in hover. Experiments in Fluids (pp 1-14) 54, 1600 (2013) 10.1007/s00348-013-1600-9
  • Baars, W. J., Tinney, C. E. Transient wall pressures in an over expanded and large area ratio nozzle. Experiments in Fluids (pp 1-17) 54, 1468 (2013) 10.1007/s00348-013-1468-8
  • Dolder, C. N., Haberman, M .R., Tinney, C. E. Turbulent wall pressure reduction using suction control. Experiments in Fluids (pp 1-20) 54, 1436 (2013) 10.1007/s00348-012-1436-8
  • Fi'evet, R., Tinney, C. E., Murray, N. E., Lyons, G., Panickar, P. Acoustic source indicators using LES in a fully expanded and heated supersonic jet. 19th AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2013-2193 (2013). Berlin, Germany.
  • Baars, W. J., Tinney, C. E. Quantifying crackle-inducing acoustic shock-structures emitted by a fully-expanded Mach 3 jet. 19th AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2013-2081 (2013). Berlin, Germany.
  • Baars, W. J., Tinney, C.E. Temporal and spectral quantification of the Crackle component in supersonic jet noise. 2nd Symposium on Fluid-Structure-Sound Interactions and Control, (eds. Zhou, Y., Liu, Y., Huang, L., Hodges, D. H., Hong-Kong, PRC, (pp 205-210) 10.1007/978-3-642-40371-2_30
  • Stephenson, J. H., Tinney, C. E., Watts, M. Time frequency analysis of sound from a maneuvering rotorcraft. American Helicopter Society 69th Annual Forum. (2017). Phoenix, USA.

2012 (9) up arrow to top of list

  • Dolder, C. N., Haberman, M .R., Tinney, C. E. A laboratory scale piezoelectric array for underwater measurements of the fluctuating wall pressure beneath turbulent boundary layers. Measurement Science Technology Journal, IOP Publishing (pp 1-11) 23, 4 (2012) 10.1088/0957-0233/23/4/045901
  • Baars, W. J., Tinney, C. E., Ruf, J. H., Brown, A. M., McDaniels, D. M. Wall pressure unsteadiness and side loads in overexpanded rocket nozzles. AIAA Journal (pp 61-73) 50, 1 (2012) 10.2514/1.J051075
  • Murray, N., Lyons, G., Tinney, C. E., Donald, B., Baars, W., Thurow, B., Haynes, H., Panickar, P. A laboratory framework for synchronous near/far-field acoustics and MHz PIV in high-temperature, shock-containing jets. Proceedings of the Internoise 2012/ASME NCAD meeting, (pp 505-519) (2012). New York City, USA.10.1115/NCAD2012-1270
  • Karpatne, A., Sirohi, J., Mula, S. M., Tinney, C. E. Investigation of tip vortex aperiodicity in hover. American Helicopter Society 68th Annual Forum. (2012). Fort Worth, USA.
  • Mula, S. M., Stephenson, J., Tinney, C. E., Sirohi, J. Dynamical and evolutionary characteristics of the tip vortex from a four bladed rotor in hover. American Helicopter Society 68th Annual Forum. (2012). Fort Worth, USA.
  • Villanueva, M. A., Tinney, C. E., Dolder, C. N., Haberman, M. R. Flowfield and wall pressure characteristics downstream of a boundary layer suction device. 50th AIAA Aerospace Sciences Meeting and Exposition, AIAA Paper 2012-0743 (2012). Nashville, USA.
  • Donald. B. W., Baars, W. J., Tinney, C. E., Ruf, J. H. Acoustic characterization of sub-scale rocket nozzles. 50th AIAA Aerospace Sciences Meeting and Exposition, AIAA Paper 2012-0544 (2012). Nashville, USA.
  • Stephenson, J. H., Mula, S. M., Tinney, C. E., Sirohi, J. Far wake rotorcraft vortex tumbling. 50th AIAA Aerospace Sciences Meeting and Exposition, AIAA Paper 2012-0425 (2012). Nashville, USA.
  • Baars, W. J., Tinney, C. E., Wochner, M. S. Nonlinear noise propagation from a fully expanded Mach 3 jet. 50th AIAA Aerospace Sciences Meeting and Exposition, AIAA Paper 2012-1177 (2012). Nashville, USA.

2011 (4) up arrow to top of list

  • Baars, W. J., Tinney, C. E., Ruf, J.H. Time-frequency analysis of rocket nozzle wall pressure during start-up transients. Proceedings of the 13th European Turbulence Conference, Warsaw, Poland. Online proceedings at: http://etc13.fuw.edu.pl/papers/proceedings
  • Mula, S. M., Stephenson, J., Tinney, C. E., Sirohi, J. Vortex jitter in hover. American Helicopter Society Southwest Regional Technical Specialists Meeting. (2011). Fort Worth, USA.
  • Baars, W. J., Tinney, C. E., Murray, N. E., Jansen, B. J., Panickar, P. The effect of heat on turbulent mixing noise in supersonic jets. 49th AIAA Aerospace Sciences Meeting and Exposition, AIAA Paper 2011-1029 (2011). Orlando, USA.
  • Dolder, C. N., Haberman, M. R., Villanueva, M. A., Tinney, C. E. Turbulent pressure signature reduction using turbulent boundary layer suction control. 49th AIAA Aerospace Sciences Meeting and Exposition, AIAA Paper 2011-0751 (2011). Orlando, USA.

2010 (4) up arrow to top of list

  • Baars, W.J., Stearman, R.O., Tinney, C.E. A review on the impact of icing on aircraft stability and control. Journal of Aeroelasticity and Structural Dynamics (pp 35-52) 2, 1 (2010) 10.3293/asdj.2010.7
  • Baars, W.J., Tinney, C.E., Ruf, J. H., Brown, A. M., McDaniels, D.M. On the unsteadiness associated with shock-induced separation in overexpanded rocket nozzles. 46th AIAA Joint Propulsion Conference and Exhibit, AIAA Paper 2010-6728 (2010). Nashville, USA.
  • Stephenson, J., Tinney, C.E., Sirohi, J. The near-field pressure of a small-scale rotor during hover. 48th AIAA Aerospace Sciences Meeting and Exposition, AIAA Paper 2010-0008 (2010). Orlando, USA.
  • Baars, W.J., Tinney, C.E., Powers, E. POD based spectral Higher-Order Stochastic Estimation. (2010). 48th AIAA Aerospace Sciences Meeting and Exposition, AIAA Paper 2010-1292 (2010). Orlando, USA.

2009 (4) up arrow to top of list

  • Tinney, C. E., Ukeiley, L. S. A study of a 3-D double backward facing step. Experiments in Fluids (pp 427-438) 47, 3 (2009) 10.1007/s00348-009-0675-9
  • Baars, W. J., Stearman, R. O., Tinney, C.E. Wind tunnel studies employing higher order statistics to detect icing induced upsets. International Forum on Aeroelasticity and Structural Dynamics, Paper 2009-0012 (2009). Seattle, USA.
  • Baars, W. J., Tinney, C. E., Stearman, R. O. Higher-order statistical analysis of stability upsets induced by elevator horn icing. 27th AIAA Applied Aerodynamics Conference, AIAA Paper 2009-3770 (2009). San Antonio, USA.
  • Tinney, C. E. Proper grid resolutions for the proper basis. 47th AIAA Aerospace Sciences Meeting and Exposition, AIAA Paper 2009-0068 (2009). Orlando, USA.

2008 (8) up arrow to top of list

  • Tinney, C. E., Ukeiley, L. S., Glauser, M. N. Low-dimensional characteristics of a transonic jet. Part 2: Estimate and far-field prediction. Journal of Fluid Mechanics (pp 53-92) 615 (2008) 10.1017/S0022112008003601
  • Tinney, C. E., Glauser, M. N., Ukeiley, L. S. Low-dimensional characteristics of a transonic jet. Part 1: Proper Orthogonal Decomposition. Journal of Fluid Mechanics (pp 107-141) 612 (2008) 10.1017/S0022112008002978
  • Tinney, C. E., Jordan, P. The near pressure field of co-axial subsonic jets. Journal of Fluid Mechanics (pp 175-204) 611 (2008) 10.1017/S0022112008001833
  • Dudley, J., Shumway, G., Tinney, C. E., Ukeiley, L. Flow characteristics of the University of Florida-REEF Supersonic Wind Tunnel. 38th AIAA Fluid Dynamics Conference, AIAA Paper 2008-3942 (2008). Seattle, USA.
  • Khambatta, P., Ukeiley, L., Tinney, C. E., Stanford, B., Ifju, P. Flow characteristics of a three-dimensional fixed micro air vehicle wing. 38th AIAA Fluid Dynamics Conference, AIAA Paper 2008-3820 (2008). Seattle, USA.
  • Guitton, A., Jordan, P., Delville, J., Tinney, C. E., Kerherv'e, F., Fortun'e, V., Gervais, Y. Experimental investigations of the velocity field and the near field pressure of a coaxial subsonic jet. Proceedings of the 7th International Symposium on Engineering Turbulence Modelling and Measurements. (2008) Limassol, Cyprus.
  • Hall, J. W., Tinney, C. E., Ausser, J. M., Pinier, J. T., Hall, A. M., Glauser, M. N. Low-dimensional tools for closed-loop flow control in high Reynolds-number turbulent flows. IUTAM Symposium on Flow Control and MEMS, (ed. Morrison, J.F., Birch, D.M., Lavoie, P., (2008) London, England.
  • Kerherv'e, F., Guitton, A., Jordan, P., Delville, J., Fortun'e, V., Gervais, Y., Tinney, C. E. Identifying the dynamics underlying the large-scale jet noise similarity spectra. 29th AIAA Aeroacoustics Conference, AIAA Paper 2008-3027 (2008). Vancouver, Canada.

2007 (6) up arrow to top of list

  • Ukeiley, L. S., Tinney, C. E., Mann, R., Glauser, M. N. Spatial correlations in a transonic jet. AIAA Journal (pp 1357-1369) 45, 6 (2007). 10.2514/1.26071
  • Tinney, C. E., Jordan, P., Delville, J., Hall, A.M., Glauser, M.N. A time-resolved estimate of the turbulence and sound source mechanisms in a subsonic jet flow. Journal of Turbulence (pp 1-20) 8, 7 (2007). 10.1080/14685240600928472
  • Tinney, C. E., Jordan, P. Coupling mechanisms in a co-axial transonic jet. 28th AIAA Aeroacoustics Conference, AIAA Paper 2007-3649 (2007). Rome, Italy.
  • Tinney, C. E., Glauser, M. N. The Modified Complementary Technique applied to the Mach 0.85 axisymmetric jet for noise prediction. 28th AIAA Aeroacoustics Conference, AIAA Paper 2007-3663 (2007). Rome, Italy.
  • Jordan, P., Schlegel, M., Stalnov, O., Noack, B., Tinney, C. E. Identifying noisy and quiet modes in a jet. 28th AIAA Aeroacoustics Conference, AIAA Paper 2007-3602 (2007). Rome, Italy.
  • Guitton, A., Tinney, C. E., Jordan, P., Delville, J. Measurements in a co-axial subsonic jet. 45th AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper 2007-0015 (2007). Reno, USA.

2006 (5) up arrow to top of list

  • Tinney, C. E., Coiffet, F., Delville, J., Glauser, M., Jordan, P., Hall, A. On spectral linear stochastic estimation. Experiments in Fluids (pp 763-775) 41, 5 (2006). 10.1007/s00348-006-0199-5
  • Tinney, C. E., Glauser, M. N., Eaton E., Taylor, J. A. Low-dimensional azimuthal characteristics of suddenly expanding axisymmetric flows. Journal of Fluid Mechanics (pp 141-155) 567 (2006) 10.1017/S0022112006002527
  • Higuchi, H., van Langen, P., Sawada, H., Tinney, C. E. Axial flow over a blunt circular cylinder with and without shear layer reattachment. Journal of Fluids and Structures (pp 949-959) 22 (2006). 10.1016/j.jfluidstructs.2006.04.020
  • Tinney, C. E., Jordan, P., Guitton, A., Delville, J., Coiffet, F. A study in the near pressure field of co-axial subsonic jets. 27th AIAA Aeroacoustics Conference, AIAA Paper 2006-2589 (2006). Boston, USA.
  • Tinney, C. E., Jordan, P., Delville, J., Hall, A. M., Glauser M. N. A time-resolved estimate of the turbulence and source mechanisms in a subsonic jet flow. 44th AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper 2006-0621 (2006). Reno, USA.