| Year |
Citation |
Score |
| 2017 |
Alfred J, Celi R, Leishman JG. Flight Path Optimization for Brownout Mitigation Using a High-Fidelity Simulation Model Journal of the American Helicopter Society. 62: 1-15. DOI: 10.4050/Jahs.62.032012 |
0.369 |
|
| 2015 |
Rand O, Khromov V, Hersey S, Celi R, Juhasz O, Tischler MB. Linear inflow model extraction from high-fidelity aerodynamic models for flight dynamics applications Annual Forum Proceedings - Ahs International. 3: 1909-1924. |
0.753 |
|
| 2014 |
Juhasz O, Syal M, Celi R, Khromov V, Rand O, Ruzicka GC, Strawn RC. Comparison of three coaxial aerodynamic prediction methods including validation with model test data Journal of the American Helicopter Society. 59. DOI: 10.4050/Jahs.59.032006 |
0.757 |
|
| 2014 |
Tritschler JK, Celi R, Leishman JG. Methodology for rotorcraft brownout mitigation through flight path optimization Journal of Guidance, Control, and Dynamics. 37: 1524-1553. DOI: 10.2514/1.G000330 |
0.767 |
|
| 2014 |
Hersey S, Sridharan A, Celi R. Multiobjective performance optimization of a coaxial compound rotorcraft configuration American Helicopter Society International - 5th Decennial Ahs Aeromechanics Specialists' Conference 2014: Current Challenges and Future Directions in Rotorcraft Aeromechanics. 450-461. DOI: 10.2514/1.C033999 |
0.327 |
|
| 2014 |
Juhasz O, Ivler CM, Tischler MB, Celi R. Control of a large flexible tiltrotor aircraft in Hover American Helicopter Society International - Rotorcraft Handling Qualities Specialists' Meeting 2014. 61-82. |
0.71 |
|
| 2013 |
Tritschler J, Celi R. Brownout cloud characterization using the modulation transfer function Journal of the American Helicopter Society. 58. DOI: 10.4050/Jahs.58.012001 |
0.312 |
|
| 2013 |
Nelson H, Celi R. Analysis of helicopter flight dynamics through modeling and simulation of primary flight control actuation system Annual Forum Proceedings - Ahs International. 1: 530-549. |
0.314 |
|
| 2013 |
Alfred J, Celi R, Leishman JG. Rotorcraft brownout mitigation through flight path optimization using a high fidelity rotorcraft simulation model Annual Forum Proceedings - Ahs International. 3: 1837-1856. |
0.358 |
|
| 2012 |
Juhasz O, Celi R, Ivler CM, Tischler MB, Berger T. Flight dynamic simulation modeling of large flexible tiltrotor aircraft Annual Forum Proceedings - Ahs International. 2: 1441-1471. |
0.758 |
|
| 2012 |
Tritschler J, Syal M, Celi R, Leishman JG. The effect of number of blades on optimum rotor design for brownout mitigation American Helicopter Society International - Future Vertical Lift Aircraft Design Conference 2012. 250-269. |
0.348 |
|
| 2011 |
Tritschler JK, Celi R. Ground-level measurements of the modulation transfer function of a brownout cloud 37th European Rotorcraft Forum 2011, Erf 2011. 10-18. |
0.732 |
|
| 2010 |
Tritschler J, Celi R. The use of the modulation transfer function for brownout cloud characterization Journal of the American Helicopter Society. 55: 0450011-0450014. DOI: 10.4050/Jahs.55.045001 |
0.314 |
|
| 2010 |
Tritschler JK, Syal M, Celi R, Leishman JG. A methodology for rotorcraft brownout mitigation using rotor design optimization Annual Forum Proceedings - Ahs International. 2: 1378-1394. |
0.776 |
|
| 2010 |
Juhasz O, Syal M, Celi R, Khromov V, Rand O, Ruzicka GC, Strawn RC. A comparison of three coaxial aerodynamic prediction methods including validation with model test data Ahs Aeromechanics Specialists Conference 2010. 528-547. |
0.751 |
|
| 2007 |
Celi R. Rotorcraft dispatching in large-scale emergencies using sequential linear assignment techniques Annual Forum Proceedings - Ahs International. 2: 1266-1279. DOI: 10.4050/Jahs.55.032004 |
0.37 |
|
| 2007 |
Malpica C, Celi R. Simulation-based bandwidth analysis of a swashplateless rotor helicopter Annual Forum Proceedings - Ahs International. 3: 2021-2042. |
0.377 |
|
| 2006 |
Lovera M, Colaneri P, Malpica C, Celi R. Closed-loop aeromechanical stability of hingeless rotor helicopters with higher harmonic control Journal of Guidance, Control, and Dynamics. 29: 179-189. DOI: 10.2514/1.7949 |
0.767 |
|
| 2006 |
Fusato D, Celi R. Multidisciplinary design optimization for aeromechanics and handling qualities Journal of Aircraft. 43: 241-252. DOI: 10.2514/1.7943 |
0.751 |
|
| 2006 |
Ribera M, Celi R. Simulation modeling in climbing and descending flight with refined aerodynamics Annual Forum Proceedings - Ahs International. 1048-1079. |
0.355 |
|
| 2005 |
Celi R. State-space representation of vortex wakes using the method of lines 30th European Rotorcraft Forum. 2005: 55-67. DOI: 10.4050/1.3092855 |
0.377 |
|
| 2005 |
Cheng RP, Celi R. Optimum two-per-revolution inputs for improved rotor performance Journal of Aircraft. 42: 1409-1417. DOI: 10.2514/1.20884 |
0.74 |
|
| 2005 |
Ribera M, Celi R. Simulation modeling in steady turning flight with refined aerodynamics 31st European Rotorcraft Forum. 2005. |
0.321 |
|
| 2004 |
Lovera M, Colaneri P, Celi R. On the role of zeros in rotorcraft aeromechanics Journal of the American Helicopter Society. 49: 318-327. DOI: 10.4050/Jahs.49.318 |
0.442 |
|
| 2004 |
Lovera M, Colaneri P, Malpica C, Celi R. Discrete-time, closed-loop aeromechanical stability analysis of helicopters with higher harmonic control Annual Forum Proceedings - American Helicopter Society. 2: 2060-2076. DOI: 10.2514/1.13874 |
0.783 |
|
| 2004 |
Gaiani G, Lovera M, Colaneri P, Celi R. Discrete-time analysis of HHC schemes for helicopter vibration attenuation Ifac Proceedings Volumes. 37: 69-74. DOI: 10.1016/S1474-6670(17)31445-3 |
0.373 |
|
| 2004 |
Ribera M, Celi R. Simulation modeling of unsteady maneuvers using a time accurate free wake Annual Forum Proceedings - American Helicopter Society. 2: 1798-1817. |
0.316 |
|
| 2003 |
Cheng RP, Theodore CR, Celi R. Effects of two/rev higher harmonic control on rotor performance Journal of the American Helicopter Society. 48: 18-27. DOI: 10.4050/Jahs.48.18 |
0.748 |
|
| 2003 |
Fusato D, Celi R. Design Sensitivity Analysis for Helicopter Flight Dynamic and Aeromechanic Stability Journal of Guidance, Control, and Dynamics. 26: 918-927. DOI: 10.2514/2.6919 |
0.734 |
|
| 2003 |
Celi R. Stabilization of helicopter blades with severed pitch links using trailing-edge flaps Journal of Guidance, Control, and Dynamics. 26: 585-592. DOI: 10.2514/2.5086 |
0.404 |
|
| 2002 |
Theodore C, Celi R. Helicopter flight dynamic simulation with refined aerodynamics and flexible blade modeling Journal of Aircraft. 39: 577-586. DOI: 10.2514/2.2995 |
0.783 |
|
| 2001 |
Fusato D, Guglieri G, Celi R. Flight dynamics of an articulated rotor helicopter with an external slung load Journal of the American Helicopter Society. 46: 3-13. DOI: 10.4050/Jahs.46.3 |
0.727 |
|
| 2000 |
Celi R. Solution of rotary-wing aeromechanical problems using differential-algebraic equation solvers Journal of the American Helicopter Society. 45: 253-262. DOI: 10.4050/Jahs.45.253 |
0.32 |
|
| 2000 |
Jones CT, Celi R. Frequency response sensitivity functions for helicopter frequency domain system identification Ibm Journal of Research and Development. 44: 748-758. DOI: 10.4050/Jahs.42.244 |
0.329 |
|
| 2000 |
Celi R. Optimization-based inverse simulation of a helicopter slalom maneuver Journal of Guidance, Control, and Dynamics. 23: 289-297. DOI: 10.2514/2.4521 |
0.418 |
|
| 1999 |
Huang CY, Celi R, Shih IC. Reconfigurable flight control systems for a tandem rotor helicopter Journal of the American Helicopter Society. 44: 50-62. DOI: 10.4050/Jahs.44.50 |
0.335 |
|
| 1998 |
Guglieri G, Celi R. Some aspects of helicopter flight dynamics in steady turns Journal of Guidance, Control, and Dynamics. 21: 383-390. DOI: 10.2514/2.4270 |
0.434 |
|
| 1997 |
Sahasrabudhe V, Celi R, Tits AL. Integrated rotor-flight control system optimization with aeroelastic and handling qualities constraints Journal of Guidance, Control, and Dynamics. 20: 217-224. DOI: 10.2514/2.4034 |
0.423 |
|
| 1997 |
Sahasrabudhe V, Celi R. Efficient treatment of moderate amplitude constraints for helicopter handling qualities design optimization Journal of Aircraft. 34: 730-739. DOI: 10.2514/2.2251 |
0.394 |
|
| 1997 |
Turnour SR, Celi R. Effects of unsteady aerodynamics on the flight dynamics of an articulated rotor helicopter Journal of Aircraft. 34: 187-196. DOI: 10.2514/2.2171 |
0.422 |
|
| 1997 |
Guglieri G, Celi R. On some aspects of helicopter flight dynamics and handling qualities in steady turns 22nd Atmospheric Flight Mechanics Conference. 524-535. |
0.315 |
|
| 1996 |
Turnour SR, Celi R. Modeling of flexible rotor blades for helicopter flight dynamics applications Journal of the American Helicopter Society. 41: 52-61. DOI: 10.4050/Jahs.41.52 |
0.464 |
|
| 1996 |
Shih IC, Spence AM, Celi R. Semianalytical sensitivity of Floquet characteristic exponents with application to rotary-wing aeroelasticity Journal of Aircraft. 33: 322-330. DOI: 10.2514/3.46941 |
0.392 |
|
| 1995 |
Spence AM, Celi R. Coupled Rotor-Fuselage Dynamics and Aeroelasticity in Turning Flight Journal of the American Helicopter Society. 40: 47-58. DOI: 10.4050/Jahs.40.47 |
0.366 |
|
| 1994 |
Ingle SJ, Celi R. Effects of Higher Order Dynamics on Helicopter Flight Control Law Design Journal of the American Helicopter Society. 39: 12-23. DOI: 10.4050/Jahs.39.12 |
0.368 |
|
| 1994 |
Spence AM, Celi R. Efficient Sensitivity Analysis for Rotary-Wing Aeromechanical Problems Aiaa Journal. 32: 2337-2344. DOI: 10.2514/3.12297 |
0.432 |
|
| 1993 |
Kim FD, Celi R, Tischler MB. Forward flight trim and frequency response validation of a helicopter simulation model Journal of Aircraft. 30: 854-863. DOI: 10.2514/3.46427 |
0.422 |
|
| 1991 |
Celi R. Hingeless Rotor Dynamics in Coordinated Turns Journal of the American Helicopter Society. 36: 39-47. DOI: 10.4050/Jahs.36.39 |
0.354 |
|
| 1991 |
Celi R. Effect of Hingeless Rotor Aeroelasticity on Helicopter Longitudinal Flight Dynamics Journal of the American Helicopter Society. 36: 35-44. DOI: 10.4050/Jahs.36.35 |
0.386 |
|
| 1991 |
Celi R. Optimum Aeroelastic Design of Helicopter Rotors for Longitudinal Handling Qualities Improvement Journal of Aircraft. 28: 49-57. DOI: 10.2514/3.45991 |
0.449 |
|
| 1991 |
Celi R. Helicopter rotor blade aeroelasticity in forward flight with an implicit structural formulation Aiaa Journal. 30: 2274-2282. DOI: 10.2514/3.11215 |
0.353 |
|
| 1990 |
Celi R, Friedmann PP. Structural optimization with aeroelastic constraints of rotor blades with straight and swept tips Aiaa Journal. 28: 928-936. DOI: 10.2514/3.25141 |
0.395 |
|
| 1988 |
Celi R, Friedmann PP. Rotor blade aeroelasticity in forward flight with an implicit aerodynamic formulation Aiaa Journal. 26: 1425-1433. DOI: 10.2514/3.10060 |
0.31 |
|
| 1987 |
Celi R, Friedmann PP. AEROELASTIC MODELING OF SWEPT TIP ROTOR BLADES USING FINITE ELEMENTS Annual Forum Proceedings - American Helicopter Society. 1: 257-269. DOI: 10.4050/Jahs.33.43 |
0.408 |
|
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