Shreyas Ananthan : Curriculum Vitae

[1]
S. Ananthan and J. Baeder, “Prediction and validation of loads on bearingless rotors using a coupled CFD-CSD methodology,” in ANNUAL FORUM PROCEEDINGS-AMERICAN HELICOPTER SOCIETY, 2008, vol. 64, p. 188.
[2]
S. Ananthan, J. Baeder, S. Hahn, G. Iaccarino, and B. Sim, “Prediction and Validation of the Aerodynamics, Structural Dynamics, and Acoustics of the SMART Rotor Using a Loosely-Coupled CFD-CSD Analysis,” in American Helicopter Society 66th Annual Forum, Phoenix, AZ, 2010.
[3]
C. C. Hennes, H.-N. Chen, K. S. Brentner, S. Ananthan, and J. G. Leishman, “Influence of Transient Flight Maneuvers on Rotor Wake Dynamics and Noise Radiation,” in Annual Forum Proceedings-American Helicopter Society, 2004, vol. 2, p. 1.
[4]
J. Leishman, M. Bhagwat, and S. Ananthan, “Free-vortex wake predictions of the vortex ring state for single-rotor and multi-rotor configurations,” in AHS International, 58 th Annual Forum Proceedings-, 2002, vol. 1, pp. 642–671.
[5]
S. Ananthan and J. G. Leishman, “Helicopter rotor wake dynamics during simulated tactical maneuvers,” in Annual Forum Proceedings-American Helicopter Society, 2004, vol. 1, pp. 949–980.
[6]
S. Ananthan, J. D. Baeder, J. Sitaraman, S. Hahn, and G. Iaccarino, “Hybrid Unsteady Simulation of Helicopters: HUSH,” in AIAA Paper, 2008, vol. 7339, p. 2008.
[7]
S. Ananthan, “Analysis of rotor wake aerodynamics during maneuvering flight using a free-vortex wake methodology,” Ph.D., University of Maryland, College Park, MD, 2006.
[8]
S. Hahn, G. Iaccarino, S. Ananthan, and J. D. Baeder, “Extension of CHIMPS for unstructured overset simulation and higher-order interpolation,” 2009.
[9]
A. Mishra, S. Ananthan, and J. D. Baeder, “Coupled CFD/CSD Prediction of the Effects of Trailing Edge Flaps on Rotorcraft Dynamic Stall Alleviation,” 2009.
[10]
A. Abhishek, A. Datta, S. Ananthan, and I. Chopra, “Prediction, Analysis, and Validation of Main Rotor Blade Loads in a Prescribed Pull-Up Maneuver,” 2009.
[11]
G. Iaccarino et al., “DARPA Helicopter Quieting Program W911NF0410424,” MARYLAND UNIV COLLEGE PARK OFFICE OF RESEARCH ADMINISTRATION AND ADVANCEMENT, 2009.
[12]
H. Chen, K. S. Brentner, S. Ananthan, and J. G. Leishman, “A Computational Study of Helicopter Rotor Wakes and Noise Generated During Transient Maneuvers,” Journal of the American Helicopter Society, vol. 53, no. 1, pp. 37–55, 2008.
[13]
D. A. Griffiths, S. Ananthan, and J. G. Leishman, “Predictions of rotor performance in ground effect using a free-vortex wake model,” Journal of the American Helicopter Society, vol. 50, no. 4, pp. 302–314, 2005.
[14]
S. Thomas, S. Ananthan, and J. D. Baeder, “Wake-Coupling CFD-CSD Analysis of Helicopter Rotors in Steady and Maneuvering Flight Conditions,” AHS Specialist’s Conference on Aeromechanics, 2010.
[15]
A. Abhishek, S. Ananthan, J. Baeder, and I. Chopra, “Prediction and Fundamental Understanding of Stall Loads in UH-60A Pull-Up Maneuver,” Journal of the American Helicopter Society, vol. 56, no. 4, pp. 1–14, 2011.
[16]
J. Baeder et al., “DARPA Helicopter Quieting Program W911NF0410424,” DTIC Document, 2009.
[17]
S. Ananthan and J. G. Leishman, “Role of Filament Strain in the Free-Vortex Modeling of Rotor Wakes,” Journal of the American Helicopter Society, vol. 49, no. 2, pp. 176–191, 2004.
[18]
S. Ananthan, J. G. Leishman, and M. Ramasamy, “The role of filament stretching in the free-vortex modeling of rotor wakes,” Annual Forum Proceedings-American Helicopter Society, vol. 58, no. 2, pp. 2005–2022, 2002.
[19]
J. G. Leishman and S. Ananthan, “Aerodynamic Optimization of a Coaxial Proprotor,” Annual Forum Proceedings-American Helicopter Society, vol. 62, no. 1, p. 64, 2006.
[20]
H. Chen, K. S. Brentner, J. Shirey, J. Horn, S. Ananthan, and J. G. Leishman, “A Study of the Aerodynamics and Acoustics of Super-BVI,” ANNUAL FORUM PROCEEDINGS-AMERICAN HELICOPTER SOCIETY, vol. 62, no. 2, p. 798, 2006.
[21]
A. Abhishek, A. Datta, S. Ananthan, and I. Chopra, “Prediction and Analysis of Main Rotor Loads in a Prescribed Pull-Up Maneuver,” Journal of Aircraft, vol. 47, no. 4, pp. 1197–1215, 2010.
[22]
J. G. Leishman and S. Ananthan, “An optimum coaxial rotor system for axial flight,” Journal of the American Helicopter Society, vol. 53, no. 4, pp. 366–381, 2008.
[23]
S. Ananthan and J. Leishman, “Predictions of Transient Rotor Wake Aerodynamics in Response to Time-Dependent Blade Pitch Inputs,” ANNUAL FORUM PROCEEDINGS-AMERICAN HELICOPTER SOCIETY, vol. 59, no. 2, pp. 1741–1762, 2003.
[24]
S. Ananthan and J. G. Leishman, “Rotor wake aerodynamics in large amplitude maneuvering flight,” Journal of the American Helicopter Society, vol. 51, no. 3, pp. 225–243, 2006.
[25]
J. G. Leishman, M. J. Bhagwat, and S. Ananthan, “The vortex ring state as a spatially and temporally developing wake instability,” Journal of the American Helicopter Society, vol. 49, no. 2, pp. 160–175, 2004.
[26]
S. ANANTHAN and J. G. LEISHMAN, “Transient helicopter rotor wakes in response to time-dependent blade pitch inputs,” Journal of aircraft, vol. 41, no. 5, pp. 1025–1041, 2004.