Year |
Citation |
Score |
2016 |
Pirau S, Liberi B, Barbely N, Komerath N. Aerodynamic load maps of bluff bodies: Measurement and diagnostics Journal of Mechanical Science and Technology. 30: 3961-3967. DOI: 10.1007/S12206-016-0808-Z |
0.32 |
|
2015 |
Raghav V, Komerath N. Advance ratio effects on the flow structure and unsteadiness of the dynamic-stall vortex of a rotating blade in steady forward flight Physics of Fluids. 27: 27101. DOI: 10.1063/1.4906803 |
0.349 |
|
2014 |
Gregory JW, Disotell KJ, Peng D, Juliano TJ, Crafton J, Komerath NM. Inverse methods for deblurring pressure-sensitive paint images of rotating surfaces Aiaa Journal. 52: 2045-2061. DOI: 10.2514/1.J052793 |
0.331 |
|
2014 |
Disotell KJ, Peng D, Juliano TJ, Gregory JW, Crafton JW, Komerath NM. Single-Shot temperature- And pressure-Sensitive paint measurements on an unsteady helicopter blade Experiments in Fluids. 55. DOI: 10.1007/S00348-014-1671-2 |
0.378 |
|
2014 |
Raghav V, Komerath N. Velocity measurements on a retreating blade in dynamic stall Experiments in Fluids. 55: 1669. DOI: 10.1007/S00348-014-1669-9 |
0.382 |
|
2013 |
Raghav V, Komerath N. An Exploration of Radial Flow on a Rotating Blade in Retreating Blade Stall Journal of the American Helicopter Society. 58: 1-10. DOI: 10.4050/Jahs.58.022005 |
0.371 |
|
2013 |
Raghav V, Komerath N. Instability of the radial flow over a rotating disk in a separated edgewise stream Physics of Fluids. 25: 111701. DOI: 10.1063/1.4833435 |
0.332 |
|
2013 |
Sharma S, Raghav V, Komerath N, Smith M. Wall effect on fluid–structure interactions of a tethered bluff body Physics Letters A. 377: 2079-2082. DOI: 10.1016/J.Physleta.2013.06.002 |
0.338 |
|
2013 |
Raghav V, Shenoy R, Smith M, Komerath N. Investigation of drag and wake turbulence of a rotor hub Aerospace Science and Technology. 28: 164-175. DOI: 10.1016/J.Ast.2012.10.012 |
0.404 |
|
2012 |
Komerath NM, Pant R, Kar A. An architecture using lighter-than-air platforms for retail power beaming and communications Journal of Low Power Electronics. 8: 261-269. DOI: 10.1166/Jolpe.2012.1190 |
0.32 |
|
2012 |
Komerath N, Kar A. Retail beamed power using millimeter waves: Survey Acm Journal On Emerging Technologies in Computing Systems. 8: 18. DOI: 10.1145/2287696.2287701 |
0.307 |
|
2011 |
Komerath NM, Smith MJ, Tung C. A review of rotor wake physics and modeling Journal of the American Helicopter Society. 56. DOI: 10.4050/Jahs.56.022006 |
0.324 |
|
2011 |
Komerath NM, Komerath PP. Terrestrial micro renewable energy applications of space technology Physics Procedia. 20: 255-269. DOI: 10.1016/J.Phpro.2011.08.024 |
0.311 |
|
2007 |
Wanis SS, Rangedera T, Komerath NM. Particle-particle interaction in electromagnetic fields for force-field tailoring Aip Conference Proceedings. 880: 177-184. DOI: 10.1063/1.2437454 |
0.747 |
|
2006 |
Gregory JW, Sullivan JP, Wanis SS, Komerath NM. Pressure-sensitive paint as a distributed optical microphone array. The Journal of the Acoustical Society of America. 119: 251-61. PMID 16454281 DOI: 10.1121/1.2140935 |
0.737 |
|
2006 |
Komerath N, Satyshur P, Rangedera T, Wanis S. System Design of Large Space Structures Using Tailored Force Fields Space. DOI: 10.2514/6.2006-7323 |
0.754 |
|
2006 |
Boechler N, Hameer S, Wanis S, Komerath N. An evolutionary model for space solar power Aip Conference Proceedings. 813: 1189-1196. DOI: 10.1063/1.2169301 |
0.735 |
|
2006 |
Wanis SS, Komerath NM. Validation of tailored force fields concept for use in space-based construction Aip Conference Proceedings. 813: 1170-1177. DOI: 10.1063/1.2169299 |
0.765 |
|
2006 |
Vasilescu R, Ganesh B, Dancila DS, Komerath NM, Sankar LN. Geometry tip cap effects on formation and near wake evolution of the rotor tip vortices Collection of Technical Papers - 36th Aiaa Fluid Dynamics Conference. 2: 1306-1319. |
0.606 |
|
2005 |
Vanmali R, Tomlinson B, Li B, Wanis S, Komerath N. Engineering a Space Based Construction Robot Sae Transactions. 114: 1375-1382. DOI: 10.4271/2005-01-3406 |
0.762 |
|
2005 |
Vanmali R, Li B, Tomlinson B, Zaidi W, Wanis S, Komerath N. Conceptual Design of a Multipurpose Robotic Craft for Space Based Construction Space. DOI: 10.2514/6.2005-6733 |
0.755 |
|
2004 |
Wanis SS, Komerath NM. Use of Radiation Pressure for Space-Based Construction Engineering Construction and Operations in Challenging Environments Earth and Space 2004: Proceedings of the Ninth Biennial Asce Aerospace Division International Conference. 317-324. |
0.763 |
|
1999 |
Wanis S, Sercovich AH, Komerath NM. Acoustic shaping in microgravity: Higher order surface shapes 37th Aerospace Sciences Meeting and Exhibit. |
0.768 |
|
1998 |
Affes H, Xiao Z, Conlisk AT, Kim JM, Komerath NM. Model for rotor tip vortex-airframe interaction part 3: Viscous flow on airframe Aiaa Journal. 36: 409-415. DOI: 10.2514/2.378 |
0.358 |
|
1998 |
Reddy UC, Matos CM, Mahalingam R, Funk RB, Komerath NM. Velocity measurement in a rotor wake interacting with a fixed wing 36th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.303 |
|
1997 |
Darden LA, Komerath N. Aircraft control using stagnation point displacement Sae Technical Papers. DOI: 10.4271/975590 |
0.342 |
|
1997 |
Komerath NM, Ames RG, Magill JC. Expanding the role of the wind-driven manipulator Sae Technical Papers. DOI: 10.4271/975589 |
0.362 |
|
1997 |
Mahalingam R, Funk RB, Komerath NM. Low speed canard-tip-vortex airfoil interaction Sae Technical Papers. DOI: 10.4271/971469 |
0.383 |
|
1996 |
Magill JC, Darden LA, Komerath NM. Flow visualization during multiple-axis motions using a wind-driven manipulator Journal of Aircraft. 33: 163-170. DOI: 10.2514/3.46917 |
0.35 |
|
1996 |
Hubner JP, Komerath NM. Counter-rotating structures over a delta wing Aiaa Journal. 34: 1958-1960. DOI: 10.2514/3.13337 |
0.302 |
|
1995 |
Foley SM, Funk RB, Fawcett PA, Komerath NM. Rotor-wake-induced flow separation on a lifting surface Journal of the American Helicopter Society. 40: 24-27. DOI: 10.4050/Jahs.40.24 |
0.351 |
|
1995 |
Lal MK, Liou SG, Pierce GA, Komerath NM. Correlation of Unsteady Pressure and Inflow Velocity Fields of a Pitching Rotor Blade Journal of Aircraft. 32: 520-528. DOI: 10.2514/3.46751 |
0.382 |
|
1995 |
Hubner JP, Komerath NM. Spectral Mapping of Quasiperiodic Structures in a Vortex Flow Journal of Aircraft. 32: 493-500. DOI: 10.2514/3.46747 |
0.357 |
|
1995 |
Kim JM, Komerath NM. Summary of the interaction of a rotor wake with a circular cylinder Aiaa Journal. 33: 470-478. DOI: 10.2514/3.12600 |
0.36 |
|
1994 |
Kim JM, Komerath NM, Liou SG. Vorticity concentration at the edge of the inboard vortex sheet Journal of the American Helicopter Society. 39: 30-34. DOI: 10.4050/Jahs.39.30 |
0.374 |
|
1994 |
Liou SG, Komerath NM, Lal MK. Measurement around a rotor blade excited in pitch, Part 1: Dynamic flow Journal of the American Helicopter Society. 39: 3-12. DOI: 10.4050/Jahs.39.2.3 |
0.331 |
|
1994 |
Lal MK, Liou SG, Pierce GA, Komerath NM. Measurement around a rotor blade excited in pitch, Part 2: Unsteady surface pressure Journal of the American Helicopter Society. 39: 13-20. DOI: 10.4050/Jahs.39.13 |
0.37 |
|
1993 |
Affes H, Conlisk AT, Kim JM, Komerath NM. Model for rotor tip vortex-airframe interaction. II - Comparison with experiment Aiaa Journal. 31: 2274-2282. DOI: 10.2514/3.11925 |
0.336 |
|
1993 |
Komerath NM, Kim JM, Liou SG. Rotor wake interaction with separated flow Mathematical and Computer Modelling. 18: 73-87. DOI: 10.1016/0895-7177(93)90105-8 |
0.383 |
|
1992 |
Komerath NM, Liou SG, Schwartz RJ, Kim JM. Flow over a twin-tailed aircraft at angle of attack. II - Temporal characteristics Journal of Aircraft. 29: 413-420. DOI: 10.2514/3.46177 |
0.351 |
|
1991 |
Komerath NM, Mavris DM, Liou SG. Prediction of unsteady pressure and velocity over a rotorcraft in forward flight Journal of Aircraft. 28: 509-516. DOI: 10.2514/3.46056 |
0.409 |
|
1990 |
Brand AG, McMahon HM, Komerath NM. Correlations of Rotor Wake/Airframe Interaction Measurements with Flow Visualization Data Journal of the American Helicopter Society. 35: 4-15. DOI: 10.4050/Jahs.35.4 |
0.397 |
|
1990 |
Liou SG, Komerath NM, Mcmahon HM. Velocity field of a cylinder in the wake of a rotor in forward flight Journal of Aircraft. 27: 804-809. DOI: 10.2514/3.45940 |
0.411 |
|
1990 |
Liou SG, Komerath NM, McMahon HM. Measurement of the interaction between a rotor tip vortex and a cylinder Aiaa Journal. 28: 975-981. DOI: 10.2514/3.25153 |
0.384 |
|
1989 |
Mavris DN, Komerath NM, McMahon HM. Prediction of aerodynamic rotor-airframe interactions in forward flight Journal of the American Helicopter Society. 34: 37-46. DOI: 10.4050/Jahs.34.37 |
0.367 |
|
1989 |
Brand A, Komerath N, Mcmahon H. Results from laser sheet visualization of a periodic rotor wake Journal of Aircraft. 26: 438-443. DOI: 10.2514/3.45782 |
0.37 |
|
1989 |
Liou SG, Komerath NM, McMahon HM. Velocity measurements of airframe effects on a rotor in low-speed forward flight Journal of Aircraft. 26: 340-348. DOI: 10.2514/3.45766 |
0.387 |
|
1989 |
Brand AG, McMahon HM, Komerath NM. Surface pressure measurements on a body subject to vortex wake interaction Aiaa Journal. 27: 569-574. DOI: 10.2514/3.10147 |
0.37 |
|
1988 |
Thompson TL, Komerath NM, Gray RB. Visualization and measurement of the tip vortex core of a rotor blade in hover Journal of Aircraft. 25: 1113-1121. DOI: 10.2514/3.45710 |
0.374 |
|
1988 |
Brand AG, Komerath NM, McMahon HM. Laser sheet technique for visualizing a periodic rotor wake Journal of Aircraft. 25: 667-669. DOI: 10.2514/3.45640 |
0.364 |
|
1985 |
Komerath NM, Hegde UG, Strahle WC. TURBULENT STATIC PRESSURE FLUCTUATIONS AWAY FROM FLOW BOUNDARIES Aiaa Journal. 23: 1320-1326. DOI: 10.2514/3.9087 |
0.671 |
|
1985 |
Chandran SBS, Komerath NM, Grissom WM, Jagoda JI, Strahle WC. Time resolved thermometry by simultaneous thermocouple and rayleigh scattering measurements in a turbulent flame Combustion Science and Technology. 44: 47-60. DOI: 10.1080/00102208508960292 |
0.639 |
|
Low-probability matches (unlikely to be authored by this person) |
2006 |
Komerath NM, Rangedera T, Nally J. Space-based economy valuation, analysis, and refinement Collection of Technical Papers - Space 2006 Conference. 1: 44-53. DOI: 10.2514/6.2006-7204 |
0.298 |
|
1997 |
Darden LA, Komerath NM. Relationship between stagnation point deflection and forebody vortex asymmetry Aiaa Journal. 35: 1892-1894. DOI: 10.2514/2.51 |
0.298 |
|
2013 |
Shenoy R, Holmes M, Smith MJ, Komerath NM. Scaling evaluations on the drag of a hub system Journal of the American Helicopter Society. 58. DOI: 10.4050/Jahs.58.032002 |
0.296 |
|
1995 |
Lee J, Xiao Z, Burggraf OR, Conlisk AT, Komerath NM. An inviscid analysis of vortex surface collisions 1995 Fluid Dynamics Conference. 1-12. |
0.295 |
|
2007 |
Komerath N, Nally J, Tang EZ. Policy model for space economy infrastructure Acta Astronautica. 61: 1066-1075. DOI: 10.1016/J.Actaastro.2006.12.033 |
0.288 |
|
1996 |
Magill JC, Komerath NM, Dorsey JF. Experimental evaluation of an adaptive controller for a wind-driven pitch manipulator Journal of Guidance, Control, and Dynamics. 19: 671-679. DOI: 10.2514/3.21673 |
0.284 |
|
1993 |
Affes H, Conlisk AT, Kim JM, Komerath NM. Model for rotor tip vortex-airframe interaction, Part 2: Comparison with experiment Aiaa Journal. 31: 2274-2282. |
0.282 |
|
1988 |
Komerath NM, Thompson TL, Kwon OJ, Gray RB. Velocity field of a lifting rotor blade in hover Journal of Aircraft. 25: 250-257. |
0.28 |
|
1995 |
Mahalingam R, Peterson KG, Funk R, Komerath NM, Conlisk AT. Recent experiments on vortex collisions with a cylinder 1995 Fluid Dynamics Conference. 1-17. |
0.278 |
|
2018 |
Shukla D, Komerath N. Multirotor Drone Aerodynamic Interaction Investigation Drones. 2: 43. DOI: 10.3390/DRONES2040043 |
0.277 |
|
1997 |
Mahalingam R, Komerath NM, Radcliff TD, Burggraf OR, Conlisk AT. Vortex-surface collision: 3-D core flow effects 28th Fluid Dynamics Conference. |
0.274 |
|
1995 |
Komerath NM, Fawcett PA, Funk RB, Reddy UC. Large-area velocity measurement in low-speed flows Iciasf Record, International Congress On Instrumentation in Aerospace Simulation Facilities. |
0.271 |
|
2013 |
Barbely NL, Pirau SI, Komerath NM. Measurements of wall formation forces in an acoustic resonator Asme International Mechanical Engineering Congress and Exposition, Proceedings (Imece). 2. DOI: 10.1115/IMECE2013-63307 |
0.269 |
|
1996 |
Komerath N. Experimental Curriculum in Diagnostics and Control of Unsteady Flows Journal of Engineering Education. 85: 263-268. DOI: 10.1002/J.2168-9830.1996.Tb00242.X |
0.269 |
|
1996 |
Mahalingam R, Funk RB, Komerath NM. Flow visualization of low speed perpendicular vortex-airfoil interaction 14th Applied Aerodynamics Conference. |
0.268 |
|
1999 |
Reddy UC, Komerath NM. 3D velocity field measurement in large-scale rotor flows 30th Fluid Dynamics Conference. |
0.264 |
|
1995 |
Hubner JP, Komerath NM. Modification of spectral characteristics in a vortex flow field 13th Applied Aerodynamics Conference. 265-275. |
0.259 |
|
1998 |
Reddy UC, Komerath NM. Whole-field velocity measurement for rotorcraft aerodynamic interactions Annual Forum Proceedings - American Helicopter Society. 1: 419-431. |
0.257 |
|
2012 |
Disotell KJ, Juliano TJ, Peng D, Gregory JW, Crafton J, Komerath NM. Unsteady pressure-sensitive paint measurements on an articulated model helicopter in forward flight 28th Aiaa Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference 2012. |
0.252 |
|
2002 |
Ganesh BA, Komerath NM. Large-scale construction for a space-based economy Space 2002 and Robotics 2002. 531-537. |
0.25 |
|
1985 |
Komerath NM, Thompson TL, Gray RB. VELOCITY MEASUREMENTS IN THE NEAR WAKE OF A HOVERING ROTOR American Society of Mechanical Engineers (Paper). |
0.247 |
|
2017 |
Schatzman NL, Komerath N, Romander EA. Time-Varying Loads of Co-Axial Rotor Blade Crossings Sae International Journal of Aerospace. 10: 68-76. DOI: 10.4271/2017-01-2024 |
0.245 |
|
1992 |
Komerath NM, Schwartz RJ, Kim JM. Flow over a twin-tailed aircraft at angle of attack, part II. Temporal characteristics Journal of Aircraft. 29: 553-558. |
0.245 |
|
1995 |
Darden LA, Peterson KG, Komerath NM. Vortex control using a moveable nose with pressure feedback 20th Atmospheric Flight Mechanics Conference. 393-403. |
0.242 |
|
2006 |
Shelton A, Tomar A, Prasad JVR, Smith MJ, Komerath N. Active Multiple Winglets for Improved Unmanned-Aerial-Vehicle Performance Journal of Aircraft. 43: 110-116. DOI: 10.2514/1.13987 |
0.24 |
|
1998 |
Mahalingam R, Komerath NM. Measurements of the near wake of a rotor in forward flight 36th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.24 |
|
2019 |
Shukla D, Komerath N. An Experimental Investigation of Rotor–Box Aerodynamic Interaction1 Journal of Fluids Engineering. 141. DOI: 10.1115/1.4043951 |
0.237 |
|
1997 |
Darden LA, Villarreal L, Komerath NM. Time scales of forebody vortex response 4th Shear Flow Control Conference. |
0.23 |
|
1985 |
Komerath NM, McMahon HM, Hubbartt JE. AERODYNAMIC INTERACTIONS BETWEEN A ROTOR AND AIRFRAME IN FORWARD FLIGHT American Society of Mechanical Engineers (Paper). |
0.228 |
|
2011 |
Raghav V, Komerath NM. Physics of transient stall on a rotating blade due to blockage Imeti 2011 - 4th International Multi-Conference On Engineering and Technological Innovation, Proceedings. 1: 45-50. |
0.228 |
|
2013 |
Raghav V, Mayo M, Lozano R, Komerath N. Evidence of vortex-induced lift on a yawed wing in reverse flow Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 228: 2130-2137. DOI: 10.1177/0954410013511597 |
0.227 |
|
1992 |
Komerath NM, Liou SG, Schwartz RJ, Kim JM. Flow over a twin-tailed aircraft at angle of attack. Part I. Spatial characteristics Journal of Aircraft. 29: 413-420. |
0.226 |
|
1998 |
Darden LA, Villarreal L, Komerath NM. Effects of wings and tunnel walls on forebody vortex asymmetry 36th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.226 |
|
1996 |
Peterson KG, Darden LA, Komerath NM. Dynamic roll control experiments using a movable nosetip 34th Aerospace Sciences Meeting and Exhibit. |
0.222 |
|
1995 |
Darden LA, Komerath NM. Forebody vortex control at high incidence using a moveable nose stagnation point 13th Applied Aerodynamics Conference. 106-116. |
0.222 |
|
2003 |
Saijo T, Ganesh B, Huang A, Komerath NM. Development of unsteadiness in a rotor wake in ground effect 21st Aiaa Applied Aerodynamics Conference. |
0.219 |
|
2018 |
Komerath N, Hiremath N, Shukla D. Testing-Based Approach to Determining the Divergence Speed of Slung Loads Aerospace. 5: 24. DOI: 10.3390/AEROSPACE5010024 |
0.218 |
|
2019 |
Shukla D, Komerath N. Drone Scale Coaxial Rotor Aerodynamic Interactions Investigation Journal of Fluids Engineering. 141. DOI: 10.1115/1.4042162 |
0.215 |
|
1997 |
Darden LA, Komerath NM. Modeling roll moment response to stagnation point actuation 22nd Atmospheric Flight Mechanics Conference. 241-251. |
0.211 |
|
1985 |
Chandran SBS, Komerath NM, Strahle WC. Scalar-velocity correlations in a turbulent premixed flame Symposium (International) On Combustion. 20: 429-435. DOI: 10.1016/S0082-0784(85)80530-0 |
0.209 |
|
2013 |
Gregory JW, Disotell KJ, Peng D, Juliano TJ, Crafton J, Komerath NM. Deconvolution-based algorithms for deblurring PSP images of rotating surfaces 51st Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2013. |
0.206 |
|
1983 |
Komerath NM, Strahle WC. MEASUREMENT OF THE PRESSURE-VELOCITY CORRELATION IN TURBULENT REACTIVE FLOWS Aiaa Paper. |
0.204 |
|
1997 |
Klein MA, Lentzt WK, Komerath NM. Reduction of fluctuations over swept wings using passive and active mini-fences 35th Aerospace Sciences Meeting and Exhibit. |
0.204 |
|
2012 |
Komerath N, Dessanti B, Shah S, Zappulla R, Picon N. Millimeter wave Space Power Grid architecture 2011 Ieee Aerospace Conference Proceedings. DOI: 10.1109/AERO.2012.6187078 |
0.203 |
|
2005 |
Ganesh B, Komerath N, Pulla D, Conlisk AT. Unsteady aerodynamics of rotorcraft in ground effect 43rd Aiaa Aerospace Sciences Meeting and Exhibit - Meeting Papers. 15229-15245. |
0.203 |
|
2014 |
Mayo M, Raghav V, Komerath N. Vortex flow hypothesis for a yawed rotor blade in reverse flow Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 229: 543-553. DOI: 10.1177/0954410014537471 |
0.2 |
|
1996 |
Ames RG, Magill JC, Komerath NM. Design and testing of a 3-d.o.f wind-driven manipulator 34th Aerospace Sciences Meeting and Exhibit. |
0.197 |
|
1996 |
Darden LA, Peterson K, Komerath NM. Roll control using a stagnation point actuator 14th Applied Aerodynamics Conference. |
0.19 |
|
1990 |
Tang W, Komerath NM, Sankar LN. Numerical simulation of the growth of instabilities in supersonic free shear layers Journal of Propulsion and Power. 6: 455-460. |
0.188 |
|
2012 |
Dessanti B, Zappulla R, Picon N, Komerath N. Design of a millimeter waveguide satellite for Space Power Grid Ieee Aerospace Conference Proceedings. DOI: 10.1109/AERO.2012.6187080 |
0.182 |
|
1990 |
Sriram P, Hanagud S, Craig J, Komerath NM. Scanning laser Doppler Technique for velocity profile sensing on a moving surface. Applied Optics. 29: 2409-17. PMID 20563182 DOI: 10.1364/Ao.29.002409 |
0.182 |
|
1997 |
Komerath NM, Hubner JP. Reply by the Authors to I. Gursul Aiaa Journal. 35: 759-759. DOI: 10.2514/2.177 |
0.173 |
|
2019 |
Hiremath N, Shukla D, Komerath N. Vortical lift on retreating rotor blades at high advance ratios Experiments in Fluids. 60. DOI: 10.1007/S00348-019-2740-3 |
0.168 |
|
2005 |
Komerath N. Global Cooperation in an Age of Security Concerns Space. DOI: 10.2514/6.2005-6638 |
0.167 |
|
2011 |
Shenoy R, Holmes M, Smith MJ, Komerath NM. Computational investigation of hub drag deconstruction from model to full scale 37th European Rotorcraft Forum 2011, Erf 2011. 684-693. |
0.164 |
|
2011 |
Komerath NM. Testbeds connecting space technology to terrestrial renewable energy Asee Annual Conference and Exposition, Conference Proceedings. |
0.16 |
|
2013 |
Komerath NM, Pendharkar AM, Raghav V. The low cost vertical axis wind turbine project: An exercise in learning across disciplines Asee Annual Conference and Exposition, Conference Proceedings. |
0.159 |
|
1995 |
Komerath NM, Magill JC. Dynamic testing in wind tunnels using the wind-driven manipulator Iciasf Record, International Congress On Instrumentation in Aerospace Simulation Facilities. |
0.158 |
|
2005 |
Ganesh B, Komerath N. Unsteady fuselage loads on rotorcraft in ground effect Sae Technical Papers. DOI: 10.4271/2005-01-3153 |
0.155 |
|
2019 |
Shukla D, Komerath N. Rotor–duct aerodynamic and acoustic interactions at low Reynolds number Experiments in Fluids. 60. DOI: 10.1007/S00348-018-2668-Z |
0.15 |
|
2011 |
Komerath NM. Advanced concept development of a hydrogen supersonic airliner: Second iteration Asee Annual Conference and Exposition, Conference Proceedings. |
0.142 |
|
1995 |
Magill JC, Komerath NM, Dorsey JF. An experimental evaluation of controllers for wind driven manipulators 20th Atmospheric Flight Mechanics Conference. 630-639. |
0.141 |
|
2003 |
Komerath NM, Gopalakrishnan P, Ganesh BA. Architecture for a radiation shielded, orbiting habitat in the earth-moon system Aiaa Space 2003 Conference and Exposition. |
0.138 |
|
2011 |
Komerath NM. Opportunities in power beaming for micro renewable energy Asee Annual Conference and Exposition, Conference Proceedings. |
0.137 |
|
2019 |
Shukla D, Komerath N. Low Reynolds number multirotor aerodynamic wake interactions Experiments in Fluids. 60. DOI: 10.1007/S00348-019-2724-3 |
0.127 |
|
2011 |
Komerath NM, Smith M, German B, Krausche DS, Armanios EA. Extrovert: Helping aerospace engineers develop advanced concepts Asee Annual Conference and Exposition, Conference Proceedings. |
0.118 |
|
2011 |
Komerath NM, German B. EXTROVERT: Experience with cross-disciplinary learning Asee Annual Conference and Exposition, Conference Proceedings. |
0.118 |
|
2014 |
Komerath N, Rangedera T, Bennett S. Extracting asteroidal mass for robotic construction Asteroids: Prospective Energy and Material Resources. 365-378. DOI: 10.1007/978-3-642-39244-3_14 |
0.11 |
|
2015 |
Raghav V, Komerath N. Dynamic Stall Life Cycle on a Rotating Blade in Steady Forward Flight Journal of the American Helicopter Society. 60: 1-12. DOI: 10.4050/jahs.60.032007 |
0.108 |
|
2013 |
Komerath NM. Renovating an ancient low speed wind tunnel: A student team project case study Asee Annual Conference and Exposition, Conference Proceedings. |
0.107 |
|
1995 |
Magill JC, Komerath NM. A WIND DRIVEN DYNAMIC MODEL MANIPULATOR FOR WIND TUNNELS Experimental Techniques. 19: 27-30. DOI: 10.1111/j.1747-1567.1995.tb00835.x |
0.1 |
|
2009 |
Sylvan R, Komerath NM, Woellert K, Homnick M, Palaia JE. The Emerging Inner Solar System Economy World Futures Review. 1: 23-38. DOI: 10.1177/194675670900100206 |
0.099 |
|
2013 |
Afman JPA, Komerath NM. Learning to innovate across disciplines: A case study on three team project experiences Asee Annual Conference and Exposition, Conference Proceedings. |
0.091 |
|
1990 |
Tang W, Komerath NM, Sankar LN. Numerical simulation of the growth of instabilities in supersonic free shear layers Journal of Propulsion and Power. 6: 455-460. DOI: 10.2514/3.25457 |
0.089 |
|
2013 |
Komerath NM. The comprehension challenge Asee Annual Conference and Exposition, Conference Proceedings. |
0.084 |
|
1983 |
Chandran SBS, Komerath NM, Grissom WM, Jagoda JI, Strahle WC. SIMULTANEOUS SENSING OF DENSITY AND TEMPERATURE IN A TURBULENT PREMIXED FLAME Chemical and Physical Processes in Combustion, Fall Technical Meeting, the Eastern States Section. |
0.081 |
|
1990 |
Komerath NM, Liou SG, Thompson TL. A REMOTE‐ALIGNED OFF‐AXIS RECEIVER FOR LASER VELOCIMETRY IN LARGE FACILITIES Experimental Techniques. 14: 29-33. DOI: 10.1111/j.1747-1567.1990.tb01110.x |
0.078 |
|
2013 |
Komerath NM. A case study on advancing learning in an upper-level engineering course Asee Annual Conference and Exposition, Conference Proceedings. |
0.073 |
|
2004 |
Komerath NM, Smith MJ. Mentoring students to technology careers Asee Annual Conference Proceedings. 9697-9707. |
0.049 |
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2021 |
Limaye S, Abedin NM, Ao CO, Bocanegra T, Bullock MA, Carrico JP, Cottini V, Curry SM, Eckles W, Elston JS, Fry PM, Gentry DM, Girija AP, Hayes AG, Jindal AS, ... ... Komerath NM, et al. Venus Observing System Bulletin of the Aas. 53. DOI: 10.3847/25C2CFEB.7E1B0BF9 |
0.047 |
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1996 |
Talukder NK, Komerath NM. Model studies on the origination of pseudo-regurgitation during heart valve closure American Society of Mechanical Engineers, Bioengineering Division (Publication) Bed. 33: 205-206. |
0.021 |
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