Year |
Citation |
Score |
2016 |
Ordaz I, Li W. Approximation of off-body sonic-boom analysis for low-boom conceptual design Journal of Aircraft. 53: 14-19. DOI: 10.2514/1.C033159 |
0.536 |
|
2015 |
Ordaz I, Geiselhart KA, Fenbert JW. Conceptual design of low-boom aircraft with flight trim requirement Journal of Aircraft. 52: 932-939. DOI: 10.2514/1.C033160 |
0.478 |
|
2015 |
Wintzer M, Ordaz I, Fenbert JW. Under-track CFD-based shape optimization for a low-boom demonstrator concept 33rd Aiaa Applied Aerodynamics Conference. |
0.571 |
|
2015 |
Ordaz I, Wintzer M, Rallabhandi SK. Full-carpet design of a low-boom demonstrator concept 33rd Aiaa Applied Aerodynamics Conference. |
0.427 |
|
2014 |
Ordaz I, Li W. Integration of off-track sonic boom analysis for supersonic aircraft conceptual design Journal of Aircraft. 51: 23-28. DOI: 10.2514/1.C031511 |
0.535 |
|
2014 |
Ordaz I, Li W, Campbell RL. Automated tetrahedral mesh generation for CFD analysis of aircraft in conceptual design 52nd Aerospace Sciences Meeting. |
0.514 |
|
2014 |
Ordaz I, Li W, Campbell RL. Automated tetrahedral mesh generation for CFD analysis of aircraft in conceptual design 52nd Aiaa Aerospace Sciences Meeting - Aiaa Science and Technology Forum and Exposition, Scitech 2014. |
0.53 |
|
2013 |
Ordaz I, Li W. Using CFD surface solutions to shape sonic boom signatures propagated from off-body pressure 31st Aiaa Applied Aerodynamics Conference. |
0.489 |
|
2013 |
Ordaz I, Li W. Advanced usage of Vehicle Sketch Pad for CFD-based conceptual design 51st Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2013. |
0.578 |
|
2012 |
Ordaz I, Liy W. Adaptive aft signature shaping of a low-boom supersonic aircraft using off-body pressures 50th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.647 |
|
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. |
0.426 |
|
2004 |
Ordaz I, Lee KH, Clark DM, Mavris DN. Aerodynamic optimization using physics-based response surface methodology for a multi-mission morphing unmanned combat air vehicle Collection of Technical Papers - Aiaa 3rd "Unmanned-Unlimited" Technical Conference, Workshop, and Exhibit. 1: 141-150. |
0.537 |
|
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