Add to ORKGSeveral aspects of the oscillating wedge are investigated to evaluate both the resulting trends for the wedge and methods of analyzing unsteady flows. An existing hypersonic small disturbance theory for an oscillating thin wedge is extended and applied. A perturbation method involving linearization about the known flow is then derived and discussed. Subsequently, a finite difference technique for calculating the complete unsteady flow field of the wedge in motion is presented and discussed in conjunction with some calculated quasi-static nonlinear trends
A finite difference code was developed for modeling inviscid, unsteady supersonic flow by solution o...
The numerical solution of flow fields behind rectangular wings is described. Subjects discussed are:...
A nonlinear, unsteady, small-disturbance theory capable of predicting inviscid transonic flows about...
In this paper an oscillating wedge has been considered, and the fluid slabs are kept at 900 to the w...
The nonlinear stability of a compressible flow past a wedge is investigated in the hypersonic limit....
The development of the flow pattern that arises during the interaction of a shock wave with a wedge ...
In this paper, analytical and numerical methods are used to evaluate flow over a wedge at supersonic...
In this paper, the shock pattern oscillations induced by shock/shock interactions over double-wedge ...
A wind-tunnel study of unsteady flow at a Mach number of 7 in helium has been conducted on several s...
A systematic study is made of the approximate inviscid theory of thin bodies moving at such high sup...
The interaction between a shock wave (attached to a wedge) and small amplitude, three-dimensional di...
A finite difference code was developed for modeling inviscid, unsteady supersonic flow by solution o...
A similitude has been obtained for an oscillating two-dimensional wedge in pitch with attached shock...
The method of integral relations is applied in a one-strip approximation to the perturbation equatio...
A semi-empirical method is developed to estimate drag on wedge-shaped projections in hypersonic flow...
A finite difference code was developed for modeling inviscid, unsteady supersonic flow by solution o...
The numerical solution of flow fields behind rectangular wings is described. Subjects discussed are:...
A nonlinear, unsteady, small-disturbance theory capable of predicting inviscid transonic flows about...
In this paper an oscillating wedge has been considered, and the fluid slabs are kept at 900 to the w...
The nonlinear stability of a compressible flow past a wedge is investigated in the hypersonic limit....
The development of the flow pattern that arises during the interaction of a shock wave with a wedge ...
In this paper, analytical and numerical methods are used to evaluate flow over a wedge at supersonic...
In this paper, the shock pattern oscillations induced by shock/shock interactions over double-wedge ...
A wind-tunnel study of unsteady flow at a Mach number of 7 in helium has been conducted on several s...
A systematic study is made of the approximate inviscid theory of thin bodies moving at such high sup...
The interaction between a shock wave (attached to a wedge) and small amplitude, three-dimensional di...
A finite difference code was developed for modeling inviscid, unsteady supersonic flow by solution o...
A similitude has been obtained for an oscillating two-dimensional wedge in pitch with attached shock...
The method of integral relations is applied in a one-strip approximation to the perturbation equatio...
A semi-empirical method is developed to estimate drag on wedge-shaped projections in hypersonic flow...
A finite difference code was developed for modeling inviscid, unsteady supersonic flow by solution o...
The numerical solution of flow fields behind rectangular wings is described. Subjects discussed are:...
A nonlinear, unsteady, small-disturbance theory capable of predicting inviscid transonic flows about...