Venkateswaran Narayanaswamy
Garcia, N., Kim, H., Vinod, K., Sahoo, A., Wax, M., Kim, T., … Jiang, X. (2024, March). Carbon nanofibers/liquid metal composites for high temperature laser ultrasound. ULTRASONICS, Vol. 138. https://doi.org/10.1016/j.ultras.2024.107245
Ramachandran, A., Sahoo, A., Narayanaswamy, V., & Lyons, K. M. (2024). Dynamics of regime transition of autoignitive jet flames from conventional to MILD combustion. APPLICATIONS IN ENERGY AND COMBUSTION SCIENCE, 19. https://doi.org/10.1016/j.jaecs.2024.100277
Johnson, E. C., & Narayanaswamy, V. (2024, September 6). High-Bandwidth Pressure Field Imaging of Stream-Traced Inlet Unstart Dynamics. AIAA JOURNAL, Vol. 9. https://doi.org/10.2514/1.J064324
Chakravarty, S., & Narayanaswamy, V. (2024). Investigations of skin friction drag mitigation over viscoelastic surfaces in supersonic flows. PHYSICAL REVIEW FLUIDS, 9(5). https://doi.org/10.1103/PhysRevFluids.9.054609
Khan, M. S. H., Madabushi, K., Ghosh, S., Edwards, J. R., & Narayanaswamy, V. (2024). Numerical investigations of shock/boundary-layer interaction and control for Mach 2.5 flow in an axisymmetric inlet. AEROSPACE SCIENCE AND TECHNOLOGY, 154. https://doi.org/10.1016/j.ast.2024.109468
Varigonda, S. V., Serafim, L. P., Freydin, M., Dowell, E. H., & Narayanaswamy, V. (2024). Two-dimensional pressure field imaging of an elastic panel executing post-flutter oscillations. JOURNAL OF FLUIDS AND STRUCTURES, 125. https://doi.org/10.1016/j.jfluidstructs.2023.104056
Walz, J., & Narayanaswamy, V. (2023). Dual separation control and drag mitigation in high speed flows using viscoelastic materials. Physics of Fluids, 35(3), 031704. https://doi.org/10.1063/5.0141572
Varigonda, S. V., & Narayanaswamy, V. (2023). Fluid structure interactions generated by an oblique shock impinging on a thin elastic panel. JOURNAL OF FLUIDS AND STRUCTURES, 119. https://doi.org/10.1016/j.jfluidstructs.2023.103890
Jenquin, C., Johnson, E. C., & Narayanaswamy, V. (2023). Investigations of shock-boundary layer interaction dynamics using high-bandwidth pressure field imaging. JOURNAL OF FLUID MECHANICS, 961. https://doi.org/10.1017/jfm.2023.168
Sahoo, A., Narayanaswamy, V., & Lyons, K. M. (2023). Quenching measurements of Kr 5p[3/2](2) <- <- 4p(61)S(0) electronic transition using absorption spectra. APPLIED OPTICS, 62(6), 110–117. https://doi.org/10.1364/AO.475382
Jenquin, C., Johnson, E., & Narayanaswamy, V. (2022). Effects of Pressure Sensitive Paint on the Dynamics of Half-Inlet Shock Dynamics. AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022, 1–13. https://doi.org/10.2514/6.2022-0068
Johnson, E., Jenquin, C., McCready, J., Narayanaswamy, V., & Edwards, J. (2022, September 30). Experimental Investigations of the Hypersonic Stream-Traced Performance Inlet at Subdesign Mach Number. AIAA JOURNAL, Vol. 61. https://doi.org/10.2514/1.J062113
Johnson, E., Jenquin, C., & Narayanaswamy, V. (2022). Experimental Studies of Unstart Shock Dynamics within a Streamtraced Scramjet Inlet. AIAA AVIATION 2022 Forum. https://doi.org/10.2514/6.2022-3478
Narayanaswamy, V., & Varigonda, S. V. (2022). Fluid Structure Interactions Generated by an Oblique Shock Impinging on a Thin Elastic Panel. SSRN. Retrieved from http://www.scopus.com/inward/record.url?eid=2-s2.0-85145488659&partnerID=MN8TOARS
Walz, J., & Narayanaswamy, V. (2022). Investigations of Shock Boundary Layer Interactions Over a Soft Material for Separated Control. AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022. https://doi.org/10.2514/6.2022-0605
Deboskey, R., Kessler, D., Johnson, R. F., Bojko, B., Sahoo, A., Narayanaswamy, V., & Lyons, K. M. (2022). Investigations of the Transition Between Conventional and Distributed Regime in Turbulent Jet Flames. AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022. https://doi.org/10.2514/6.2022-2089
Johnson, E., Jenquin, C., McCready, J., Narayanaswamy, V., & Edwards, J. (2022). Mach 4 Performance of a Hypersonic Streamtraced Inlet Part 1: Experimental Investigations. AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022. https://doi.org/10.2514/6.2022-0065
McCready, J. T., Hoppe, C. A., Johnson, E. C., Edwards, J. R., & Narayanaswamy, V. (2022). Mach 4 Performance of a Hypersonic Streamtraced Inlet – Part 2: Computational Results. AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022. https://doi.org/10.2514/6.2022-0066
Sahoo, A., Ramachandran, A., Narayanaswamy, V., & Lyons, K. M. (2022). Mixture fraction measurement in turbulent non-premixed MILD jet flame using Rayleigh scattering. Applied Optics, 61(9), 2338–2351. https://doi.org/10.1364/AO.444109
Acharya, R., Hartman, K., & Narayanaswamy, V. (2022). Multi-fidelity Reduced-Dimensional Modeling for Shock-fin Interaction. AIAA AVIATION 2022 Forum. https://doi.org/10.2514/6.2022-3479
Freydin, M., Dowell, E. H., Varigonda, S. V., & Narayanaswamy, V. (2022). Response of a plate with piezoelectric elements to turbulent pressure fluctuation in supersonic flow. JOURNAL OF FLUIDS AND STRUCTURES, 114. https://doi.org/10.1016/j.jfluidstructs.2022.103696
Peltier, S. J., Rice, B. E., Johnson, E., Narayanaswamy, V., & Sellers, M. E. (2021). Effects of three-dimensional pressure gradients on high-speed turbulent boundary layers. AIAA Scitech 2021 Forum, 1–15. Retrieved from http://www.scopus.com/inward/record.url?eid=2-s2.0-85100309661&partnerID=MN8TOARS
Boles, J., Thomas, C., Salazar, G., Edwards, J., Narayanaswamy, V., & McCready, J. (2021). Flow distortion computational modeling and design optimization for supersonic inlet. AIAA Scitech 2021 Forum, 1–21. Retrieved from http://www.scopus.com/inward/record.url?eid=2-s2.0-85100313851&partnerID=MN8TOARS
Varigonda, S. V., Jenquin, C., & Narayanaswamy, V. (2021). Impact of Panel Vibrations on the Dynamic Field Properties in Supersonic ow. AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021. https://doi.org/10.2514/6.2021-2926
Varigonda, S. V., & Narayanaswamy, V. (2021). Methodology to image the panel surface pressure power spectra in weakly coupled fluid/structure interactions. EXPERIMENTS IN FLUIDS, 62(11). https://doi.org/10.1007/s00348-021-03314-4
Freydin, M., Levin, D., Dowell, E. H., Varigonda, S. V., & Narayanaswamy, V. (2021, May). Natural Frequencies of a Heated Plate: Theory and Experiment (Sept, 10.2514/1.J059660, 2020). AIAA JOURNAL, Vol. 59, pp. AU2–AU2. https://doi.org/10.2514/1.J059660.c1
Anand Bharadwaj, S., Baskaran, S. P., Ghosh, S., & Narayanaswamy, V. (2021). Numerical investigation of passive flow control using permeable and wavy walls in oblique shock-wave/boundary-layer interaction. AIAA Scitech 2021 Forum, 1–14. Retrieved from http://www.scopus.com/inward/record.url?eid=2-s2.0-85100304482&partnerID=MN8TOARS
Pickles, J. D., Balachandra, Mettu, R., Subbareddy, P. K., Narayanaswamy, V., Vasile, J. D., & Despirito, J. (2020). Computational modeling of fin induced shock wave/turbulent boundary layer interactions over an axisymmetric surface. AIAA Scitech 2020 Forum, 1 PartF, 1–13. https://doi.org/10.2514/6.2020-1332
Pickles, J. D., & Narayanaswamy, V. (2020). Control of Fin Shock Induced Flow Separation Using Vortex Generators. AIAA JOURNAL, 58(11), 4794–4806. https://doi.org/10.2514/1.J059624
Sahoo, A., Zelenak, D., & Narayanaswamy, V. (2020). Erratum: Temperature dependence of collisional broadening and shift for the Kr 4p6S10 → 5p[3/2]2 electronic transition (Applied Optics (2020) 59 (1438–1446) DOI: 10.1364/AO.380102). Applied Optics, 59(7), 2085. https://doi.org/10.1364/AO.390320
Pickles, J. D., & Narayanaswamy, V. (2020). Investigation of Surface Curvature Effects on Unseparated Fin Shock-Wave/Boundary-Layer Interactions. AIAA JOURNAL, 58(2), 770–778. https://doi.org/10.2514/1.J058596
Leonard, M. D., & Narayanaswamy, V. (2021). Investigation of shock dynamics in an axisymmetric inlet/isolator with attached boundary layers. JOURNAL OF FLUID MECHANICS, 908. https://doi.org/10.1017/jfm.2020.899
Varigonda, S. V., Narayanaswamy, V., & Boxx, I. (2020). Investigations of fsi generated by an impinging sbli on a thin panel using multivariate imaging of flow/structural properties. AIAA AVIATION 2020 FORUM, 1 PartF. https://doi.org/10.2514/6.2020-3001
Sahoo, A., Narayanaswamy, V., Ramachandran, A., & Lyons, K. (2020). Mixture fraction imaging of distributed regime turbulent jet flame using rayleigh scattering. AIAA AVIATION 2020 FORUM, 1 PartF. https://doi.org/10.2514/6.2020-3238
Freydin, M., Levin, D., Dowell, E. H., Varigonda, S. V., & Narayanaswamy, V. (2020). Natural Frequencies of a Heated Plate: Theory and Experiment. AIAA JOURNAL, 58(11), 4969–4973. https://doi.org/10.2514/1.J059660
Ramachandran, A., Chauhan, A., Narayanaswamy, V., Lyons, K. M., & Johnson, R. (2020). On the transition of autoignitive jet flames to mild combustion. AIAA Scitech 2020 Forum, 1 PartF. https://doi.org/10.2514/6.2020-1842
Sahoo, A., Zelenak, D., & Narayanaswamy, V. (2020). Pressure scaling of the collisional broadening parameters of Kr 4p(6)S(0)(1) ->-> 5p [3/2](2) transition. APPLIED OPTICS, 59(26), 7760–7769. https://doi.org/10.1364/AO.394932
Sahoo, A., Zelenak, D., & Narayanaswamy, V. (2020). Temperature dependence of collisional broadening and shift for the Kr 4p6S10 → 5p[3/2]2 electronic transition. Applied Optics, 59(5), 1438–1446. https://doi.org/10.1364/AO.380102
Sahoo, A., & Narayanaswamy, V. (2019). 2D temperature field measurement in a sooting flame using the 2-line Kr plif thermometry technique. AIAA Aviation 2019 Forum, 1–15. https://doi.org/10.2514/6.2019-3289
Pickles, J. D., & Narayanaswamy, V. (2019). Achieving high maneuverability and precision in munitions using non-linear flow interactions. Proceedings - 31st International Symposium on Ballistics, BALLISTICS 2019, 1, 848–859. Retrieved from http://www.scopus.com/inward/record.url?eid=2-s2.0-85086429466&partnerID=MN8TOARS
Zelenak, D., & Narayanaswamy, V. (2019). Demonstration of a two-line Kr PLIF thermometry technique for gaseous combustion applications. OPTICS LETTERS, 44(2), 367–370. https://doi.org/10.1364/OL.44.000367
Funderburk, M. L., & Narayanaswamy, V. (2019, August). Experimental Investigation of Microramp Control of an Axisymmetric Shock/Boundary-Layer Interaction. AIAA JOURNAL, Vol. 57, pp. 3379–3394. https://doi.org/10.2514/1.J057846
Funderburk, M. L., & Narayanaswamy, V. (2019). Investigation of Negative Surface Curvature Effects in Axisymmetric Shock/Boundary-Layer Interaction. AIAA JOURNAL, 57(4), 1594–1607. https://doi.org/10.2514/1.J057275
Varigonda, S. V., & Narayanaswamy, V. (2019). Investigation of shock wave induced flow separation over a flexible panel in supersonic flows. AIAA Aviation 2019 Forum, 1–11. https://doi.org/10.2514/6.2019-3543
Ramachandran, A., Narayanaswamy, V., & Lyons, K. M. (2019). Observations on the Role of Auto-Ignition in Flame Stabilization in Turbulent Non-Premixed Jet Flames in Vitiated Coflow. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 141(6). https://doi.org/10.1115/1.4042807
Pickles, J. D., Mettu, B. R., Subbareddy, P. K., & Narayanaswamy, V. (2019). On the mean structure of sharp-fin-induced shock wave/turbulent boundary layer interactions over a cylindrical surface. JOURNAL OF FLUID MECHANICS, 865, 212–246. https://doi.org/10.1017/jfm.2019.53
Funderburk, M. L., & Narayanaswamy, V. (2019). Spectral signal quality of fast pressure sensitive paint measurements in turbulent shock-wave/boundary layer interactions. EXPERIMENTS IN FLUIDS, 60(10). https://doi.org/10.1007/s00348-019-2799-x
Sahoo, A., & Narayanaswamy, V. (2019). Two-dimensional temperature field imaging in laminar sooting flames using a two-line Kr PLIF approach. APPLIED PHYSICS B-LASERS AND OPTICS, 125(9). https://doi.org/10.1007/s00340-019-7280-2
Pham, H. T., Gianikos, Z. N., & Narayanaswamy, V. (2018). Compression ramp induced shock wave/turbulent boundary layer interactions on a compliant material. AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018, 56(7), 2925–2929. https://doi.org/10.2514/6.2018-0095
Pham, H. T., Gianikos, Z. N., & Narayanaswamy, V. (2018). Compression ramp induced shock-wave/turbulent boundary-layer interactions on a compliant material. AIAA Journal, 56(7), 2925–2929. https://doi.org/10.2514/1.J056652
Funderburk, M. L., & Narayanaswamy, V. (2018). Experimental investigation of microramp vortex generator application upstream of an axisymmetric shock boundary layer interaction. 2018 Joint Propulsion Conference. https://doi.org/10.2514/6.2018-4937
Pickles, J. D., Mettu, B. R., Subbareddy, P. K., & Narayanaswamy, V. (2018). Fin-generated shock wave/turbulent boundary layer interactions on a cylindrical surface with a distorted incoming boundary layer. 2018 Fluid Dynamics Conference. https://doi.org/10.2514/6.2018-3396
Pickles, J. D., Mettu, B. R., Subbareddy, P. K., & Narayanaswamy, V. (2018). Gas density field imaging in shock dominated flows using planar laser scattering. EXPERIMENTS IN FLUIDS, 59(7). https://doi.org/10.1007/s00348-018-2562-8
Leonard, M. D., & Narayanaswamy, V. (2018). Investigations of flowfield and dynamics in an axisymmetric isolator. AIAA Aerospace Sciences Meeting, 2018. https://doi.org/10.2514/6.2018-1611
Narayanaswamy, V., & Zelenak, D. (2018). Two-line Kr PLIF technique for composition independent temperature imaging in gaseous combustion. Optics InfoBase Conference Papers, Part F103-LACSEA 2018. https://doi.org/10.1364/LACSEA.2018.LTu3C.2
Zelenak, D., & Narayanaswamy, V. (2017). Composition-independent mean temperature measurements in laminar diffusion flames using spectral lineshape information. EXPERIMENTS IN FLUIDS, 58(10). https://doi.org/10.1007/s00348-017-2430-y
Funderburk, M. L., & Narayanaswamy, V. (2017). Experimental investigation of shock boundary layer interactions in axisymmetric isolator geometries. 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017. https://doi.org/10.2514/6.2017-5052
Lam, K.-Y., Pickles, J. D., Narayanaswamy, V., Carter, C. D., & Kimmel, R. L. (2017). High-speed schlieren and 10-Hz Kr PLIF for the new AFRL mach-6 Ludwieg tube hypersonic wind tunnel. AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting. https://doi.org/10.2514/6.2017-0550
Ley, K., & Narayanaswamy, V. (2017). Parametric study of forced ignition in laminar and turbulent methane jets. 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017. https://doi.org/10.2514/6.2017-4770
Pickles, J. D., Mettu, B. R., Subbareddy, P. K., & Narayanaswamy, V. (2017). Sharp-fin induced shock wave/turbulent boundary layer interactions in an axisymmetric configuration. 47th AIAA Fluid Dynamics Conference, 2017. https://doi.org/10.2514/6.2017-4314
Zelenak, D., Sealy, W., & Narayanaswamy, V. (2016). Collisional broadening of Kr (4p(6) S-0(1) -> -> 5p [3/2](2)) transition with combustion species as collision partners. Journal of Quantitative Spectroscopy & Radiative Transfer, 174, 28–38.
Zelenak, D., Sealy, W., & Narayanaswamy, V. (2016). Collisional broadening of Kr (4p6S01→→5p[32]2) transition with combustion species as collision partners. Journal of Quantitative Spectroscopy and Radiative Transfer, 174, 28–38. https://doi.org/10.1016/J.JQSRT.2016.01.017
Funderburk, M., & Narayanaswamy, V. (2016). Experimental investigation of primary and corner shock boundary layer interactions at mild back pressure ratios. PHYSICS OF FLUIDS, 28(8). https://doi.org/10.1063/1.4960963
Funderburk, M. L., & Narayanaswamy, V. (2016). Experimental investigation of shock boundary layer interactions to unravel inlet unstart physics. 46th AIAA Fluid Dynamics Conference. Retrieved from http://www.scopus.com/inward/record.url?eid=2-s2.0-84980347810&partnerID=MN8TOARS
Pickles, J. D., Subbareddy, P. K., & Narayanaswamy, V. (2016). Sharp-fin induced shock wave/turbulent boundary layer interactions in an axisymmetric configuration. 46th AIAA Fluid Dynamics Conference. https://doi.org/10.2514/6.2016-3340
Zelenak, D., Sealy, W., & Narayanaswamy, V. (2015). Composition-independent temperature and pressure measurements using lineshape information. 46th AIAA Plasmadynamics and Lasers Conference. Retrieved from http://www.scopus.com/inward/record.url?eid=2-s2.0-84960517327&partnerID=MN8TOARS
Hegde, A., Funderburk, M., Hill, J., & Narayanaswamy, V. (2015). Experimental investigation into shock induced corner boundary layer separation. 45th AIAA Fluid Dynamics Conference. https://doi.org/10.2514/6.2015-2934
Ramachandran, A., Tyler, D. A., Patel, P. K., Narayanaswamy, V., & Lyons, K. M. (2015). Global features of flame stabilization in turbulent non-premixed jet flames in vitiated coflow. 45th AIAA Fluid Dynamics Conference, 1–13. https://doi.org/10.2514/6.2015-2313
Characterization of the NASA Langley Arc Heated Scramjet Test Facility using NO PLIF. (2014). AIAA AVIATION 2014 - 30th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. https://doi.org/10.2514/6.2014-2652
Clemens, N. T., & Narayanaswamy, V. (2014). Low-Frequency Unsteadiness of Shock Wave/Turbulent Boundary Layer Interactions. ANNUAL REVIEW OF FLUID MECHANICS, VOL 46, Vol. 46, pp. 469–492. https://doi.org/10.1146/annurev-fluid-010313-141346
Gampert, M., Narayanaswamy, V., Schaefer, P., & Peters, N. (2013). Conditional statistics of the turbulent/non-turbulent interface in a jet flow. Journal of Fluid Mechanics, 731, 615–638. https://doi.org/10.1017/JFM.2013.327
Gampert, M., Schaefer, P., Narayanaswamy, V., & Peters, N. (2013). Gradient trajectory analysis in a Jet flow for turbulent combustion modelling. Journal of Turbulence, 14(1), 147–164. https://doi.org/10.1080/14685248.2012.747688
Gampert, M., Narayanaswamy, V., & Peters, N. (2013). Scalar gradient trajectory measurements using high-frequency cinematographic planar Rayleigh scattering. EXPERIMENTS IN FLUIDS, 54(12). https://doi.org/10.1007/s00348-013-1621-4
Narayanaswamy, V., & Clemens, N. T. (2013). Simultaneous LII and PIV measurements in the soot formation region of turbulent non-premixed jet flames. PROCEEDINGS OF THE COMBUSTION INSTITUTE, 34(1), 1455–1463. https://doi.org/10.1016/j.proci.2012.06.018
Narayanaswamy, V., Raja, L. L., & Clemens, N. T. (2012). Control of a shock/boundary-layer interaction by using a pulsed-plasma jet actuator. AIAA Journal, 50(1), 246–249. https://doi.org/10.2514/1.J051246
Narayanaswamy, V., Raja, L. L., & Clemens, N. T. (2012). Control of unsteadiness of a shock wave/turbulent boundary layer interaction by using a pulsed-plasma-jet actuator. Physics of Fluids, 24(7), 076101. https://doi.org/10.1063/1.4731292
Narayanaswamy, V., Burns, R., & Clemens, N. T. (2011). Kr-PLIF for scalar imaging in supersonic flows. Optics Letters, 36(21), 4185–4187. https://doi.org/10.1364/OL.36.004185
Narayanaswamy, V., Clemens, N. T., & Raja, L. L. (2011). Method for acquiring pressure measurements in presence of plasma-induced interference for supersonic flow control applications. Measurement Science and Technology, 22(12), 125107. https://doi.org/10.1088/0957-0233/22/12/125107
Hsu, A. G., Narayanaswamy, V., Clemens, N. T., & Frank, J. H. (2011). Mixture fraction imaging in turbulent non-premixed flames with two-photon LIF of krypton. Proceedings of the Combustion Institute, 33(1), 759–766. https://doi.org/10.1016/j.proci.2010.06.051
Guo, X., Zhao, H., Song, H., Combs, C., Narayanaswamy, V., Clemens, N., … Jiang, H. (2011). Upconverting nanophosphors for high temperature applications. Technical Proceedings of the 2011 NSTI Nanotechnology Conference and Expo, NSTI-Nanotech 2011, 1, 429–432. Retrieved from http://www.scopus.com/inward/record.url?eid=2-s2.0-81455133723&partnerID=MN8TOARS
Narayanaswamy, V., Raja, L. L., & Clemens, N. T. (2010). Characterization of a high-frequency pulsed-plasma jet actuator for supersonic flow control. AIAA Journal, 48(2), 297–305. https://doi.org/10.2514/1.41352
Narayanaswamy, V., Clemens, N. T., & Raja, L. L. (2010). Investigation of a pulsed-plasma jet for shock / boundary layer control. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Retrieved from http://www.scopus.com/inward/record.url?eid=2-s2.0-78649810322&partnerID=MN8TOARS
Lochman, B. J., Murphree, Z. R., Narayanaswamy, V., & Clemens, N. T. (2010). PLIF imaging of naphthalene-ablation products in a Mach 5 turbulent boundary layer. 27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference 2010, 1. https://doi.org/10.2514/6.2010-4346
Clemens, N. T., & Narayanaswamy, V. (2009). Shock/turbulent boundary layer interactions: Review of recent work on sources of unsteadiness. 39th AIAA Fluid Dynamics Conference. Retrieved from http://www.scopus.com/inward/record.url?eid=2-s2.0-78349243684&partnerID=MN8TOARS
Narayanaswamy, V., Shin, J., Clemens, N. T., & Raja, L. L. (2008). Investigation of plasma-generated jets for supersonic flow control. 46th AIAA Aerospace Sciences Meeting and Exhibit. https://doi.org/10.2514/6.2008-285
Shin, J., Narayanaswamy, V., Raja, L. L., & Clemens, N. T. (2007). Characteristics of a plasma actuator in Mach 3 flow. Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting, 14, 9665–9675. Retrieved from http://www.scopus.com/inward/record.url?eid=2-s2.0-34250798514&partnerID=MN8TOARS
Shin, J., Narayanaswamy, V., Raja, L. L., & Clemens, N. T. (2007). Characterization of a direct-current glow discharge plasma actuator in low-pressure supersonic flow. AIAA Journal, 45(7), 1596–1605. https://doi.org/10.2514/1.27197
Shin, J., Narayanaswamy, V., Raja, L. L., & Clemens, N. (2006). Generation of plasma induced flow actuation by DC glow-like discharge in a supersonic flow. Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting, 3, 2042–2051. https://doi.org/10.2514/6.2006-169
Sahoo, A., Deboskey, R., Narayanaswamy, V., & Lyons, K. (2021). 2D Velocity Field Measurement of Conventional and Distributed Regime Turbulent Jet Flame using Particle Image Velocimetry. AIAA Propulsion and Energy Forum, 2021. https://doi.org/10.2514/6.2021-3626