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Introduction to hypersonic vitrectomy
Current Opinion in Ophthalmology, 2019To review the development of hypersonic vitrectomy and present the first case series in the United States.From 27 September 2017 to 4 December 2017, 64 patients underwent hypersonic vitrectomy with 20 patients having conventional 23-ga vitrectomy for comparison.
Kevin J, Blinder +5 more
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Journal of the Aerospace Sciences, 1959
An extension of classical hypersonic similitude is developed which takes into account the interaction effect of the displacement thickness of the boundary layer. A basic result of this viscous similitude is that the total drag including frictional drag obe}^s the classical similarity law for the pressure drag. Additional similarity conditions governing
Hayes, Wallace D., Probstein, Ronald F.
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An extension of classical hypersonic similitude is developed which takes into account the interaction effect of the displacement thickness of the boundary layer. A basic result of this viscous similitude is that the total drag including frictional drag obe}^s the classical similarity law for the pressure drag. Additional similarity conditions governing
Hayes, Wallace D., Probstein, Ronald F.
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Panel flutter in hypersonic flow.
AIAA Journal, 1967IV," Transactions of the American Society for Metals, Transactions Quarterly, Vol. 59, 1966, p. 876. Fager D. N. and Spur W. F., "Some Characteristics of Aqueous Stress Corrosion in Titanium Alloys," Document D660083, Sept. 1967, The Boeing Co. 11 Beck, T. R., "Stress Corrosion Cracking of Titanium Alloys, II.
Bailie, J. A., McFeely, J. E.
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The Interaction of a Hypersonic Plume with an External Hypersonic Stream
1973Abstract : A theoretical study of the gas dynamic interaction between a hypersonic plume and the opposed hypersonic external stream is presented. Steady, axisymmetric, inviscid, perfect gas flow is postulated for both the bow and far field regions.
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Will there or will there not be a hypersonic airplane?
Journal of Engineering Physics and Thermophysics, 2000An analytical overview of the problems of heat transfer occurring in horizontal flight of a body in the earth’s atmosphere at a hypersonic speed is given. It is shown that, despite the enormous experience accumulated in the design and development of shuttle systems (Space Shuttle, Buran), the creation of a hypersonic airplane still remains a serious ...
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2015
Abstract The chapter starts its analysis with blunt-nosed bodies. In a supersonic flow, a blunt-nosed body produces a bow shock wave. The chapter shows that the shape of the shock and the entire flow between the shock and the body become independent of the Mach number, M∞, provided it is large enough.
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Abstract The chapter starts its analysis with blunt-nosed bodies. In a supersonic flow, a blunt-nosed body produces a bow shock wave. The chapter shows that the shape of the shock and the entire flow between the shock and the body become independent of the Mach number, M∞, provided it is large enough.
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1962
An experimental investigation was made of the flow field behind a two-dimensional circular cylinder at a nominal Mach number of 5.7. The free-stream Reynolds number based on the cylinder diameter was varied over a range from 4300 to 66, 500 by changing both the diameter of the cylinder and the stagnation pressure of the wind tunnel.
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An experimental investigation was made of the flow field behind a two-dimensional circular cylinder at a nominal Mach number of 5.7. The free-stream Reynolds number based on the cylinder diameter was varied over a range from 4300 to 66, 500 by changing both the diameter of the cylinder and the stagnation pressure of the wind tunnel.
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Review of Control and Guidance Technology on Hypersonic Vehicle
Chinese Journal of Aeronautics, 2022Yibo Ding, Guangshan Chen
exaly
Review of Acoustic Metasurfaces for Hypersonic Boundary Layer Stabilization
Progress in Aerospace Sciences, 2022Juanmian Lei, Chih-Yung Wen, Rui Zhao
exaly
Proposed for presentation at the Hypersonic Weapons Summit (VIRTUAL) in ,, 2021
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