| Year |
Citation |
Score |
| 2016 |
Heath CM, Slater JW, Rallabhandi SK. Inlet trade study for a low-boom aircraft demonstrator 34th Aiaa Applied Aerodynamics Conference. |
0.446 |
|
| 2015 |
Rallabhandi SK, Westy TK, Nielsenz EJ. Uncertainty analysis and robust design of low-boom concepts using atmospheric adjoints 33rd Aiaa Applied Aerodynamics Conference. |
0.46 |
|
| 2015 |
Ordaz I, Wintzer M, Rallabhandi SK. Full-carpet design of a low-boom demonstrator concept 33rd Aiaa Applied Aerodynamics Conference. |
0.557 |
|
| 2014 |
Rallabhandi SK, Nielsen EJ, Diskin B. Sonic-boom mitigation through aircraft design and adjoint methodology Journal of Aircraft. 51: 502-510. DOI: 10.2514/1.C032189 |
0.519 |
|
| 2014 |
Li W, Rallabhandi S. Inverse design of low-boom supersonic concepts using reversed equivalent-area targets Journal of Aircraft. 51: 29-36. DOI: 10.2514/1.C031551 |
0.576 |
|
| 2014 |
Rallabhandi SK. Application of adjoint methodology in various aspects of sonic boom design 32nd Aiaa Applied Aerodynamics Conference. |
0.518 |
|
| 2013 |
Rallabhandi SK. Application of adjoint methodology to supersonic aircraft design using reversed equivalent areas 31st Aiaa Applied Aerodynamics Conference. DOI: 10.2514/1.C032518 |
0.458 |
|
| 2012 |
Rallabhandi SK, Nielseny EJ, Diskin B. Sonic boom mitigation through aircraft design and Adjoint methodology 30th Aiaa Applied Aerodynamics Conference 2012. 2152-2169. |
0.521 |
|
| 2011 |
Rallabhandi SK. Sonic boom adjoint methodology and its applications 29th Aiaa Applied Aerodynamics Conference 2011. |
0.377 |
|
| 2010 |
Ordaz I, Rallabhandi SK. Boom minimization framework for supersonic aircraft using CFD analysis 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.563 |
|
| 2010 |
Rallabhandi SK, Li W, Geiselhart K. Boom-constrained drag minimization for design of supersonic concepts 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.522 |
|
| 2009 |
Plotkin KJ, Rallabhandi SK, Li W. Generalized formulation and extension of sonic boom minimization theory for front and aft shaping 47th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.478 |
|
| 2008 |
Rallabhandi SK, Mavris DN. Simultaneous airframe and propulsion cycle optimization for supersonic aircraft design 46th Aiaa Aerospace Sciences Meeting and Exhibit. DOI: 10.2514/1.33183 |
0.574 |
|
| 2007 |
Rallabhandi SK, Mavris DN. Aircraft geometry design and optimization for sonic boom reduction Journal of Aircraft. 44: 35-47. DOI: 10.2514/1.20456 |
0.536 |
|
| 2006 |
Rallabhandi SK, Mavris DN. Sonic boom minimization using inverse design and probabilistic acoustic propagation Journal of Aircraft. 43: 1815-1828. DOI: 10.2514/1.20457 |
0.499 |
|
| 2006 |
Utturwar A, Rallabhandi S, Delaurentis D, Mavris D. A two-step optimization approach for technology selection Engineering Optimization. 38: 889-908. DOI: 10.1080/03052150600795839 |
0.578 |
|
| 2006 |
Rallabhandi SK, Mavris DN. Design and analysis of supersonic business jet concepts Collection of Technical Papers - 6th Aiaa Aviation Technology, Integration, and Operations Conference. 1: 30-46. |
0.459 |
|
| 2005 |
Rallabhandi SK, Mavris DN. Sonic boom minimization using improved linearized tools and probabilistic propagation 43rd Aiaa Aerospace Sciences Meeting and Exhibit - Meeting Papers. 9753-9767. |
0.366 |
|
| 2004 |
Rallabhandi SK, Mavris DN. Sonic boom modelling under atmospheric uncertainty Collection of Technical Papers - 10th Aiaa/Issmo Multidisciplinary Analysis and Optimization Conference. 6: 3904-3914. |
0.347 |
|
| 2002 |
Utturwar A, Rallabhandi S, Delaurentis D, Mavris D. A bi-level optimization approach for technology selection 9th Aiaa/Issmo Symposium On Multidisciplinary Analysis and Optimization. |
0.543 |
|
| 2001 |
Rallabhandi SK, Cagatay E, Mavris DN. An improved procedure for prediction of drag polars of a joined wing concept using physics-based response surface methodology Sae Technical Papers. DOI: 10.4271/2001-01-3015 |
0.347 |
|
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