Zobrazeno 1 - 10
of 11
pro vyhledávání: '"Matthew A. Bennington"'
Publikováno v:
Journal of Aircraft. 42:366-375
Numerical refueling missions were simulated with a 747-400 tanker for three different sized aircraft—a 747-400, a 777-300, and an A318—to examine the impact on payload capability. Simplified performance and economic models were used to optimize t
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Experimental and computational studies were conducted to study the role of the tip leakage flow in axial compressor stall and the relationship between the tip clearance flow field and surge margin extension from circumferential groove casing treatmen
Autor:
Aspi Rustom Wadia, Song Fu, Joshua D. Cameron, Scott C. Morris, Ke Shi, Haixin Chen, Xudong Huang, Matthew A. Bennington, Mark H. Ross, Scott McNulty
Publikováno v:
Journal of Turbomachinery. 136
Numerical investigations were conducted to predict the performance of a transonic axial compressor rotor with circumferential groove casing treatment. The Notre Dame Transonic Axial Compressor (ND-TAC) was simulated at Tsinghua University with an in-
Autor:
Juan Du, Mark H. Ross, Feng Lin, Jingyi Chen, Scott C. Morris, Matthew A. Bennington, Joshua D. Cameron
Publikováno v:
Journal of Turbomachinery. 135
Experimental and numerical studies were conducted to investigate tip-leakage flow and its relationship to stall in a transonic axial compressor. The computational fluid dynamics (CFD) results were used to identify the existence of an interface betwee
Autor:
Juan Du, Joshua D. Cameron, Scott C. Morris, Jingyi Chen, Matthew A. Bennington, Mark H. Ross, Feng Lin
Publikováno v:
Volume 7: Turbomachinery, Parts A, B, and C.
A numerical and experimental study was conducted to investigate the tip clearance flow and its relationship to stall in a transonic axial compressor. The CFD results were used to identify the existence of an interface between incoming axial flow and
Autor:
Aspi Rustom Wadia, Haixin Chen, Ke Shi, Matthew A. Bennington, Scott McNulty, Xudong Huang, Song Fu, Mark H. Ross, Scott C. Morris
Publikováno v:
Volume 7: Turbomachinery, Parts A, B, and C.
Numerical investigations were conducted to predict the performance of a transonic axial compressor rotor with circumferential groove casing treatment. The Notre Dame Transonic Axial Compressor (ND-TAC) was simulated by Tsinghua University with an in-
Autor:
Matthew A. Bennington, Sean T. Barrows, Camille Legault, Jen Ping Chen, Joshua D. Cameron, Scott C. Morris, Aspi Rustom Wadia, G. Scott McNulty
Publikováno v:
Volume 6: Turbomachinery, Parts A, B, and C.
Recent stall inception investigations have indicated that short-length scale stall initiates when the interface between the tip gap flow and the approach flow spills forward of the leading edge of the adjacent blade. This hypothesis was investigated
Autor:
Aspi Rustom Wadia, G. Scott McNulty, Scott C. Morris, Matthew A. Bennington, Joshua D. Cameron
Publikováno v:
Volume 6: Turbomachinery, Parts A, B, and C.
The performance, efficiency, and stall inception of an axial compressor was investigated experimentally with small levels of rotor centerline offset. The measurements were acquired using a high-speed, single-stage compressor. The rotor was levitated
Publikováno v:
Volume 6: Turbo Expo 2007, Parts A and B.
Effects of rotor centerline offset and whirl on the pre-stall and stall inception behavior of a high-speed tip-critical axial compressor were investigated. The observations were made using a circumferential array of unsteady pressure transducers. The