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Unsteady pressure and inflow velocity on a pitching rotor blade in hoverLal, Mihir Kumar 12 1900 (has links)
No description available.
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An improved method of calculating the tip vortex geometry for hovering rotorsSamant, Satish Shripad 12 1900 (has links)
No description available.
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A method of computing the pressure distribution on a single-bladed hovering helicopter rotorShenoy, Koodige Rajarma 05 1900 (has links)
No description available.
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A theory for the analysis of rotorcraft operating in atmospheric turbulenceCostello, Mark Francis 05 1900 (has links)
No description available.
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Computational fluid dynamic studies of high lift rotor systems using distributed computingBangalore, Ashok K. 05 1900 (has links)
No description available.
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Solution procedure for the Navier-Stokes equations applied to rotorsWake, Brian E. 05 1900 (has links)
No description available.
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Combined model- and rule-based controller synthesis with application to helicopter flight controlJiang, Tian-Yue 12 1900 (has links)
No description available.
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A comprehensive approach to on-condition evaluation of rotorcraft structural integrityRees, Kevin Scott 08 1900 (has links)
No description available.
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Interfacing comprehensive rotorcraft analysis with advanced aeromechanics and vortex wake modelsLiu, Haiying. January 2007 (has links)
Thesis (Ph. D.)--Aerospace Engineering, Georgia Institute of Technology, 2008. / Committee Chair: Bauchau, Olivier; Committee Member: Armanios, Erian; Committee Member: Hodges, Dewey; Committee Member: Ruzzene, Massimo; Committee Member: Stallybrass, Michael.
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Optimal aeroelastic trim for rotorcraft with constrained, non-unique trim solutionsSchank, Troy C. January 2008 (has links)
Thesis (Ph. D.)--Aerospace Engineering, Georgia Institute of Technology, 2008. / Committee Chair: Dimitri N. Mavris; Committee Co-Chair: Daniel P Schrage; Committee Member: David A. Peters; Committee Member: Dewey H. Hodges; Committee Member: J.V.R. Prasad.
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