Results 261 to 270 of about 68,121 (308)
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Asymmetric separated flows at supersonic speeds
AIAA Journal, 1990Summary: An efficient multigrid, central difference, finite volume Navier-Stokes solver is used to study the ``natural occurrence'' of steady, anomalous, asymmetric separated ``locally conical'' flow solutions at high incidence and at supersonic speeds.
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Body-Wing Interference at Supersonic Speeds
The Journal of the Royal Aeronautical Society, 1966SummaryA summary of available information on the problem of body-wing interference in supersonic flow has shown, inter alia, that a large number of theoretical methods are available for the prediction of interference characteristics. Many of these methods are chiefly concerned with the estimation of overall characteristics,i.e.normal force and pitching
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Potential Vortex Cascades for Supersonic Speeds
1980The concept of parallel flow at the inlet and at the exit of cascades, on which, for instance, the honored’s paper referenced under [1] is based, can be realized exactly in non-viscous supersonic flow. First, the transition from parallel supersonic flow with distinct Mach numbers into potential vortex flow is defined.
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Wing-body Interference At Supersonic Speeds.
1954PhD ; Aerospace materials ; University of Michigan, Horace H. Rackham School of Graduate Studies ; http://deepblue.lib.umich.edu/bitstream/2027.42/181166/2/0007599 ...
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Lift-to-drag ratio at supersonic speeds
Fluid Dynamics, 1994Wave lift-to-drag ratio is analyzed ignoring friction and using flows behind oblique shock waves and rarefaction waves. It is shown that the lift-to-drag ratio of an infinite oblique plate can surpass considerably that of triangular plates with subsonic, sonic, or supersonic edges.
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High-speed sequential deposition of photoactive layers for organic solar cell manufacturing
Nature Energy, 2022Christoph J Brabec
exaly
Visual Problems of Supersonic Speeds
American Journal of Ophthalmology, 1951openaire +2 more sources
Flow around a cone at supersonic speed
1987In memory of the educational efforts of Prof. Chien Wei-zang, the author presents this thesis in its original form, written when he was a senior student of Tsinghua University under the guidance of Prof. Chien in the period 1947–1948. The inviscid supersonic conical flow around a cone at zero angle of attack was analysed by the method of asymptotic ...
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