| Euler-based inverse method for turbomachine blades, Part 2: Three-dimensional flows T Dang, S Damle, X Qiu AIAA journal 38 (11), 2007-2013, 2000 | 81 | 2000 |
| Euler-based inverse method for turbomachine blades. I-Two-dimensional cascades T Dang, V Isgro AIAA journal 33 (12), 2309-2315, 1995 | 64 | 1995 |
| Inverse method for turbomachine blades using shock-capturing techniques T Dang 31st Joint Propulsion Conference and Exhibit, 2465, 1995 | 63 | 1995 |
| Wind powered device PM Pelken, T Dang US Patent 7,824,060, 2010 | 37 | 2010 |
| Experimental investigation of embedded crossflow fan for airfoil propulsion/circulation control RK Dygert, TQ Dang Journal of Propulsion and Power 25 (1), 196-203, 2009 | 37 | 2009 |
| Cross-flow fan propulsion system JD Kummer, TQ Dang US Patent 7,641,144, 2010 | 36 | 2010 |
| 3D inverse method for turbomachine blading with splitter blades X Qiu, T Dang Turbo Expo: Power for Land, Sea, and Air 78545, V001T03A090, 2000 | 26 | 2000 |
| Three-dimensional viscous inverse method for axial blade design X Qiu, M Ji, T Dang Inverse Problems in Science and Engineering 17 (8), 1019-1036, 2009 | 25 | 2009 |
| Practical use of three-dimensional inverse method for compressor blade design S Damle, T Dang, J Stringham, E Razinsky | 22 | 1999 |
| Practical use of a 3d viscous inverse method for the design of compressor blade S Damle, T Dang, J Stringham, E Razinsky ASME Journal of Turbomachinery 121 (2), 321-325, 1999 | 21 | 1999 |
| Design study of turbomachine blades by optimization and inverse techniques A Nerurkar, T Dang, E Reddy, D Reddy 32nd Joint Propulsion Conference and Exhibit, 2555, 1996 | 20 | 1996 |
| Practical use of 3D inverse method for compressor blade design S Damle, T Dang, J Stringham, E Razinsky Turbo Expo: Power for Land, Sea, and Air 78620, V001T01A035, 1998 | 19 | 1998 |
| Design method for turbomachine blades with finite thickness by the circulation method J Jiang, T Dang | 15 | 1997 |
| Wind powered device PM Pelken, T Dang US Patent 8,282,236, 2012 | 12 | 2012 |
| Inverse method for turbomachine blades using existing time-marching techniques T Dang, V Isgro Turbo Expo: Power for Land, Sea, and Air 78835, V001T01A005, 1994 | 9 | 1994 |
| Numerical study of lobed-mixer fuel-injection strut in scramjet engine M Campuzano, T Dang 31st Joint Propulsion Conference and Exhibit, 2449, 1995 | 8 | 1995 |
| Computational analysis of personal ventilation jets J Russo, T Dang, HE Khalifa Indoor Air, 2008 | 6 | 2008 |
| Design method for turbomachine blades with finite thickness by the circulation method J Jiang, T Dang Turbo Expo: Power for Land, Sea, and Air 78835, V001T01A128, 1994 | 6 | 1994 |
| Evaluation of 3D Inverse Code Using Rotor 67 as Test Case T Dang | 2 | 1998 |
| Implementation of a 3D mixing layer code on parallel computers K Roe, R Thakur, T Dang, E Bogucz International Aerospace Planes and Hypersonics Technologies, 6111, 1995 | 2 | 1995 |
