Investigation of oscillating cascade aerodynamics by an experimental influence coefficient technique [PDF]
Fundamental experiments are performed in the NASA Lewis Transonic Oscillating Cascade Facility to investigate the torsion mode unsteady aerodynamics of a biconvex airfoil cascade at realistic values of the reduced frequency for all interblade phase ...
Buffum, Daniel H., Fleeter, Sanford
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Analysis of extremum seeking control for wind turbine torque controller optimization by aerodynamic and generator power objectives [PDF]
arXivWind turbines degrade over time, resulting in varying structural, aeroelastic, and aerodynamic properties. In contrast, the turbine controller calibrations generally remain constant, leading to suboptimal performance and potential stability issues. The calibration of wind turbine controller parameters is therefore of high interest. To this end, several
arxiv
Some diffuse reflection problems in radiation aerodynamics
, 1964 Stephen Nathaniel Falken
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Direct use of linear time-domain aerodynamics in aeroservoelastic analysis: Aerodynamic model [PDF]
The work presented here is the first part of a continuing effort to expand existing capabilities in aeroelasticity by developing the methodology which is necessary to utilize unsteady time-domain aerodynamics directly in aeroservoelastic design and ...
Gilbert, Michael G., Woods, J. A.
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Effect of Wind Tunnel Acoustic Modes on Linear Oscillating Cascade Aerodynamics [PDF]
, 1994 Daniel H. Buffum, Sanford Fleeter
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Unsteady aerodynamic analysis of space shuttle vehicles. Part 1: Summary report [PDF]
An analysis of the unsteady aerodynamics of space shuttle vehicles was performed. The results show that slender wing theory can be modified to give the potential flow static and dynamic characteristics over a large Mach number range from M = 0 to M 1. A
Ericsson, L. E., Reding, J. P.
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Hypersonic aerodynamics on thin bodies with interaction and upstream influence [PDF]
, 1994 A. Farid Khorrami, F. T. Smith
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Application of multidisciplinary optimization methods to the design of a supersonic transport [PDF]
An optimization design method is discussed. This method is based on integrating existing disciplinary analysis and sensitivity analysis techniques by means of generalized sensitivity equations.
Barthelemy, J.-F. M. +5 more
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Effects of Combustor Aerodynamics on the Ignition of Solid Fuel [PDF]
, 1994 Jing‐Tang Yang +2 more
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