Zobrazeno 1 - 10
of 18
pro vyhledávání: '"Steven R. Manwaring"'
Publikováno v:
Journal of Turbomachinery. 119:665-676
This paper describes a portion of an experimental and computational program (ADLARF), which incorporates, for the first time, measurements of all aspects of the forced response of an airfoil row, i.e., the flow defect, the unsteady pressure loadings,
Autor:
Sanford Fleeter, Steven R. Manwaring
Publikováno v:
Experimental Thermal and Fluid Science. 5:225-234
A series of experiments are described that are directed at the quantitative investigation of turbomachine rotor blade row unsteady unresolved velocities and blade surface pressures generated by the wakes from upstream blade and vane airfoil rows. The
Autor:
Sanford Fleeter, Steven R. Manwaring
Publikováno v:
International Journal of Turbo and Jet Engines. 8:1-16
Autor:
Steven R. Manwaring, Sanford Fleeter
Publikováno v:
Journal of Propulsion and Power. 6:590-597
Autor:
Scott D. Hunter, Steven R. Manwaring
Publikováno v:
Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery.
Axial flow turbine designers are currently using Navier-Stokes flow solvers to reveal the details of the three dimensional flowfield inside individual bladerow passages. This new capability has allowed designers to focus on secondary flow reduction t
Autor:
Michael G. Dunn, Nathan J. Heidegger, Reza S. Abhari, Michael J. Salay, Kuk K. Frey, Matthew Mark Weaver, Steven R. Manwaring
Publikováno v:
Volume 4: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education.
Reducing the vibratory stress due to the forced response excitation of turbomachinery blades is an important engineering challenge facing designers. Detailed knowledge of the unsteady forces, the damping within the system, and the structural stiffnes
Autor:
Steven R. Manwaring, Kevin L. Kirkeng
Publikováno v:
Unsteady Aerodynamics and Aeroelasticity of Turbomachines ISBN: 9789401061162
This paper presents the results of an experimental and analysis program which investigated the forced response of a low pressure turbine (LPT) blade due to circumferential temperature distortions which emanated from the combustor and propagated throu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::30f6b09423fcf8450aca00eccd1bbece
https://doi.org/10.1007/978-94-011-5040-8_25
https://doi.org/10.1007/978-94-011-5040-8_25
Publikováno v:
Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; General.
This paper describes a portion of an experimental and computational program (ADLARF) which incorporates, for the first time, measurements of all aspects of the forced response of an airfoil row, i.e., the flow defect, the unsteady pressure loadings a
Autor:
Steven R. Manwaring, Sanford Fleeter
Publikováno v:
Volume 3A: General.
Unsteady aerodynamic blade row response is generally categorized as either subresonant or superresonant, with an acoustic resonance at the points where these regions meet. Although these far field acoustic responses are critical to obtaining correct
Autor:
Sanford Fleeter, Steven R. Manwaring
Publikováno v:
Unsteady Aerodynamics, Aeroacoustics, and Aeroelasticity of Turbomachines and Propellers ISBN: 9781461393436
A series of experiments to investigate rotor unsteady aerodynamic response to high and very high reduced frequency gusts, including the effects of steady aerodynamic loading and detailed forcing function waveform shape are described. These experiment
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1954ab915caf2781cd72ecfabf6fa0eb
https://doi.org/10.1007/978-1-4613-9341-2_25
https://doi.org/10.1007/978-1-4613-9341-2_25