Anubhav Datta, Ph.D. - Publications

Affiliations: 
2004 University of Maryland, College Park, College Park, MD 
Area:
Aerospace Engineering

18 high-probability publications. We are testing a new system for linking publications to authors. You can help! If you notice any inaccuracies, please sign in and mark papers as correct or incorrect matches. If you identify any major omissions or other inaccuracies in the publication list, please let us know.

Year Citation  Score
2019 Ng W, Datta A. Hydrogen Fuel Cells and Batteries for Electric-Vertical Takeoff and Landing Aircraft Journal of Aircraft. 56: 1765-1782. DOI: 10.2514/1.C035218  0.345
2019 Staruk W, Datta A. Gimbaled Tiltrotor Conversion Flight Loads Prediction Using Three-Dimensional Structural Analysis Journal of Aircraft. 56: 758-770. DOI: 10.2514/1.C035075  0.517
2018 Staruk W, Datta A, Chopra I, Jayaraman B. An Integrated Three-Dimensional Aeromechanics Analysis of the NASA Tilt Rotor Aeroacoustic Model Journal of the American Helicopter Society. 63: 1-12. DOI: 10.4050/Jahs.63.032002  0.623
2018 Ward E, Chopra I, Datta A. Rotation-Frequency-Driven Extension–Torsion Coupled Self-Twisting Rotor Blades Journal of Aircraft. 55: 1929-1941. DOI: 10.2514/1.C034617  0.661
2016 Potsdam M, Datta A, Jayaraman B. Computational investigation and fundamental understanding of a slowed UH-60A rotor at high advance ratios Journal of the American Helicopter Society. 61. DOI: 10.4050/Jahs.61.022002  0.5
2014 Datta A, Johnson W. Powerplant Design and Performance Analysis of a Manned All-Electric Helicopter Journal of Propulsion and Power. 30: 490-505. DOI: 10.2514/1.B34843  0.376
2013 Sitaraman J, Potsdam M, Wissink A, Jayaraman B, Datta A, Mavriplis D, Saberi H. Rotor loads prediction using helios: A multisolver framework for rotorcraft aeromechanics analysis Journal of Aircraft. 50: 478-492. DOI: 10.2514/1.C031897  0.545
2011 Choi S, Datta A, Alonso JJ. Prediction of Helicopter Rotor Loads Using Time-Spectral Computational Fluid Dynamics and an Exact Fluid-Structure Interface Journal of the American Helicopter Society. 56: 1-15. DOI: 10.4050/Jahs.56.042001  0.47
2011 Datta A, Johnson W. Three-Dimensional Finite Element Formulation and Scalable Domain Decomposition for High-Fidelity Rotor Dynamic Analysis Journal of the American Helicopter Society. 56: 22003-2200314. DOI: 10.4050/Jahs.56.022003  0.307
2010 Falls J, Datta A, Chopra I. Integrated trailing-edge flaps and servotabs for helicopter primary control Journal of the American Helicopter Society. 55: 0320051-03200515. DOI: 10.4050/Jahs.55.032005  0.726
2010 Abhishek A, Datta A, Ananthan S, Chopra I. Prediction and analysis of main rotor loads in a prescribed pull-up maneuver Journal of Aircraft. 47: 1197-1215. DOI: 10.2514/1.46899  0.755
2009 Abhishek A, Datta A, Chopra I. Prediction of UH-60A structural loads using multibody analysis and swashplate dynamics Journal of Aircraft. 46: 474-490. DOI: 10.2514/1.35076  0.756
2008 Datta A, Chopra I. Prediction of the UH-60A Main Rotor Structural Loads Using Computational Fluid Dynamics/Comprehensive Analysis Coupling Journal of the American Helicopter Society. 53: 351. DOI: 10.4050/Jahs.53.351  0.698
2007 Datta A, Nixon M, Chopra I. Review of Rotor Loads Prediction with the Emergence of Rotorcraft CFD Journal of the American Helicopter Society. 52: 287. DOI: 10.4050/Jahs.52.287  0.66
2006 Datta A, Chopra I. Validation of Structural and Aerodynamic Modeling Using UH-60A Airloads Program Data Journal of the American Helicopter Society. 51: 43. DOI: 10.4050/1.3092877  0.633
2006 Datta A, Sitaraman J, Chopra I, Baeder JD. CFD/CSD prediction of rotor vibratory loads in high-speed flight Journal of Aircraft. 43: 1698-1709. DOI: 10.2514/1.18915  0.72
2004 Datta A, Chopra I. Validation and Understanding of UH-60A Vibratory Loads in Steady Level Flight Journal of the American Helicopter Society. 49: 271-287. DOI: 10.4050/Jahs.49.271  0.67
2003 Datta A, Roget B, Griffiths D, Pugliese G, Sitaraman J, Bao J, Liu L, Gamard O. Design of a Martian Autonomous Rotary-Wing Vehicle Journal of Aircraft. 40: 461-472. DOI: 10.2514/2.3141  0.695
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