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Journal Articles
46. Bellini R, Lu FK. Exergy analysis of a pulse detonation power device. Journal of Propulsion and Power, submitted.
45. Li JM, Chung KM, Lu FK. The performance assessment of pulse detonation engines in power production. Journal of Propulsion and Power, submitted.
44. Nagarajan HN, Lu FK. Thermal analysis and heat exchanger design for pulse detonation engine. International Journal of Aerospace Innovations, 1(3):145-158, 2009.
43. Massa L, Lu FK. Role of the induction region on turbulence-detonation interaction. Physics of Fluids, submitted.
42. Massa L. Spatial linear analysis of the flow in a solid rocket motor with burning walls. Combustion and Flame 156(4):865-888, 2009.
41. Lu FK, Ortiz AA, Li J, Kim CH, Chung K. Detection of shock and detonation wave propagation by cross correlation. Mechanical Systems and Signal Processing, 23(4):1098-1111, 2009.
40. Lu FK, Wilson DR, Matsumoto J. Rapid valve opening technique for a supersonic blowdown tunnel. Experimental Thermal and Fluid Science, 33(3):551-554, 2009.
39. Braun EM, Lu FK, Wilson DR. Experimental research in aerodynamic control with electric and electromagnetic fields. Progress in Aerospace Sciences, 45(1-3):30-49, 2009.
38. Li JM, Lai WH, Chung KM, Lu FK. Experimental study on transmission of an overdriven detonation wave from propane/oxygen to propane/air.Combustion and Flame, 154(3):331-345, 2008.
37. Fan HY, Lu FK. Numerical analysis of the tube-in-tube type PDE mode. International Journal of Turbo & Jet Engines, 25(4):233-246, 2008.
36. Fan HY, Lu FK. Numerical modelling of oblique shock and detonation waves induced in a wedged channel. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 222(5):687-703, 2008.
35. Fan HY, Lu FK. Numerical simulation of detonation processes in a variable cross-section chamber. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 222(5):673-686, 2008.
34. Emanuel G. Vorticity in unsteady, viscous, reacting flow and downstream of a curved shock. AIAA Journal, 45(8):2097–2099, 2007.
33. Emanuel G, Hekiri H. Vorticity and its rate of change just downstream of a curved shock. Shock Waves, 17(1-2):85-94, 2007
32. Abolmaali A, Treadway J, Aswath P, Lu FK, McCarthy E. Hysteresis behavior of T-stub connections with superelastic shape memory smart fasteners. Journal of Steel Construction Research, 62(8):831–838, 2006.
31. Lu FK, Fan HY, Wilson DR. Detonation waves induced by a confined wedge. Aerospace Science and Technology, 10(8):679–685, 2006.
30. Li J, Chung K, Lai W, Lu FK. Uncertainty analysis of deflagration-to-detonation run-up distance. Shock Waves, 14(5-6):413–420, 2005.
29. Emanuel G, Satyanand US, Lu FK. Performance of a shock tube with a large area contraction. AIAA Journal, 43(9):1995–1999, 2005.
28. Lu FK, Liu HC, Wilson DR. Electrical conductivity channel for a shock tube. Measurement Science and Technology, 16(9):1730–1740, 2005.
27. Terrier DE, Lu FK. Aerodynamically controlled expansion nozzle for STOVL aircraft. Journal of Propulsion and Power, 21(4):763–765, 2005.
26. Fan HY, Lu FK. Comparison of detonation processes in a variable cross-section chamber and a simple tube. Journal of Propulsion and Power, 21(1):65–75, 2005.
25. Kim HY, Lu FK, Anderson DA, Wilson DR. Numerical simulation of detonation process in a tube. CFD Journal, 12(2):227–241, 2003.
24. Lu FK, Terrier DE. Performance analysis of short takeoff and vertical landing aircraft nozzle in hover. Journal of Propulsion and Power, 19(4):715–717, 2003.
23. Lu FK, Wilson DR. Detonation driver for enhancing shock tube performance. Shock Waves, 12(6):457–468, 2003.
22. Lu FK, Kim HY, McNay LN. A simplified trajectory analysis model for small satellite pay-load recovery from low earth orbit. Aerospace Science and Technology, 7(3):231–237, 2003.
21. Lu FK, Wilson DR, Bakos RJ, Erdos JI. Recent advances in detonation techniques for high-enthalpy facilities. AIAA Journal, 38(9):1676–1684, 2000.
20. Lu FK, Kinnear KM. Characterization of thin film heat flux gauges. Journal of Thermophysics and Heat Transfer, 13(4):548–550, 1999.
19. Lu FK, Zhang X. Visualization of a confined accelerated bubble. Shock Waves, 9(5):333–339, 1999.
18. Lu FK, Liu X. On the optical design of Cranz-Schardin cameras. Optical Engineering, 36(7):1935–1941, 1997.
17. Chung KM, Lu FK. Hypersonic turbulent expansion-corner flow with shock impingement. Journal of Propulsion and Power, 11(3):441-447, 1995.
16. Bigdeli B, Lu FK. Hypersonic, turbulent viscous interaction past an expansion corner. AIAA Journal, 32(9):1815-1819, 1994.
15. Magnusson R, Wang X, Hafiz A, Black TD, Tello LN, Haji-Sheikh A, Konecni S, Wilson DR. Experiments with photorefractive crystals for holographic interferometry. Optical Engineering, 33(2):596-607, 1994.
14. Chung KM, Lu FK. Damping of surface pressure fluctuations in hypersonic turbulent flow past expansion corners. AIAA Journal, 31(7):1229-1234, 1993.
13. Lu FK. Quasiconical free interaction between a swept shock and a turbulent boundary layer. AIAA Journal, 31(4):686-692, 1993.
12. Kalkhoran IM, Wilson DR, Seath DD. Experimental investigation of the perpendicular rotor blade-vortex interaction at transonic speeds. AIAA Journal, 30(3):747-755, 1992.
11. Kalkhoran IM, Wilson DR. Experimental investigation of the parallel rotor blade-vortex interaction at transonic speeds. AIAA Journal, 30(8):2087-2092, 1992.
10. Lu FK, Chung KM. Downstream influence scaling of turbulent flow past expansion corners. AIAA Journal, 30(12):2976-2977, 1992.
9. Lu FK, Settles GS. On the upstream-influence scaling of sharp fin interactions. AIAA Journal, 29(7):1180-1181, 1991.
8. Lu FK, Settles GS. Inception length to a fully-developed fin-generated shock wave boundary-layer interaction. AIAA Journal, 29(5):758-762, 1991.
7. Lu FK, Settles GS. Color surface-flow visualization of fin-generated shock-wave boundary-layer interactions. Experiments in Fluids, 8:352-354, 1990.
6. Lu FK, Settles GS, Horstman CC. Mach number effects on conical surface features of swept shock boundary-layer interactions. AIAA Journal, 28(1):91-97, 1990.
5. Seath DD, Kim JM, Wilson DR. Investigation of parallel blade-vortex interaction at low speed. Journal of Aircraft, 26(4):328-333, 1989.
4. Hafiz A, Magnusson R, Bagby JS, Wilson DR, Black TD. Visualization of aerodynamic flow fields using photorefractive crystals. Applied Optics, 28(8):1521-1524, 1989.
3. Jung Y, Seath DD. Spanwise displacement of a line vortex above a wing - a simple calculation scheme. Journal of Aircraft, 25(5):476-478, 1988.
2. Settles GS, Hsu JC, Metwally OM, Lu FK. Visualization of high-speed flows at the Penn State Gas Dynamics Laboratory. Proceedings of the Laser Institute of America, 67:95-104, 1988.
1. Mitchell JH, Magnusson R, Black TD, Wilson DR. Holographic interferometry using iron-doped lithium niobate. Applied Physics Letters, 51(2):81-82, July 13, 1987.
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