Zobrazeno 1 - 10
of 37
pro vyhledávání: '"Wing-Fai Ng"'
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Publikováno v:
Journal of Propulsion and Power. 16:216-226
Experiments were performed to study the effects of toe-in angle on the exterior ports of a three-hole, lowdownstream-angleinjector array in a supersonic e ow. The three jetswere arranged e ush with the test section e oor so that the interference betw
Publikováno v:
Bit Numerical Mathematics. 40:24-40
In this paper, we consider solving non-convolution type integral equations by the preconditioned conjugate gradient method. The fast dense matrix method is a fast multiplication scheme that provides a dense discretization matrix A approximating a giv
Publikováno v:
International Journal for Numerical Methods in Engineering. 43:1505-1521
In this paper, we consider solving potential equations by the boundary integral equation approach. The equations so derived are Fredholm integral equations of the first kind and are known to be ill-conditioned. Their discretized matrices are dense an
Publikováno v:
52nd Aerospace Sciences Meeting.
The motion and evolution of coherent structures in supersonic jet flows is directly related to the intense noise the flow generates. As a preliminary study to experimentally address these relationships, novel non-intrusive measurements using two-comp
Publikováno v:
52nd Aerospace Sciences Meeting.
Supersonic jet noise is a major health concern in military aviation which may be alleviated with physicsbased control strategies. In order to understand the physics of sound generation from supersonic free jets, highly resolved experimental investiga
Publikováno v:
Journal of Turbomachinery. 135
An experimental study was performed to measure surface Nusselt number and film cooling effectiveness on a film cooled first stage nozzle guide vane (NGV) at high freestream turbulence, using a transient thin film gauge (TFG) technique. The informatio
Publikováno v:
Volume 7: Structures and Dynamics, Parts A and B.
Erosion and deposition in gas turbine engines are functions of particle/wall interactions and Coefficient of Restitution (COR) is a fundamental property of these interactions. COR depends on impact velocity, angle of impact, temperature, particle com