Results 71 to 80 of about 789,848 (154)
Laminar and Turbulent Aero Heating Predictions over Blunt Body in Hypersonic Flow [PDF]
فصلنامه علوم و فناوری فضایی, 2014 In the present work, an engineering method is developed to predict laminar and turbulent heating-rate solutions for blunt reentry spacecraft at hypersonic conditions.
S. A. Hosseini, S. Noori
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Aerothermodynamics issues of the DLR hypersonic flight experiment SHEFEX-I [PDF]
, 2008 Here is presented an overview of the hypersonic experiment on sharp edge concepts, SHEFEX-I. The project, being performed under responsibility of the German Aerospace Center (DLR), is aimed to investigate the behavior and the possibilities of an improved
Eggers, Thino +2 more
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Local correlation-based transition model for aerodynamic flows in wide speed range
Engineering Applications of Computational Fluid MechanicsA local correlation-based transition model is developed for aerodynamic flows in a wide speed range. New localized methods for the momentum-thickness Reynolds number are introduced for constructing local transition indicators. New transition correlations
Hexia Huang, Zaijie Liu, Huijun Tan
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Future Prospects for Hypersonic Flight Test For University Students [PDF]
, 2005 The transport to space of satellites and experiments with conventional expandable rockets is a very expensive and time demanding business and therefore almost prohibitive for Universities and High-School or Colleges laboratories.
Behrens, J. +3 more
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FlowBase-flow computations and stability analyses are performed for a hypersonic wind tunnel nozzle at a Mach number of 6. Isothermal and adiabatic wall boundary conditions are investigated, and moderate stagnation conditions are used to provide ...
Hugo Lemarquand +5 more
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Advances in Mechanical Engineering, 2019 At hypersonic speeds, the external wall temperatures of an aerospace vehicle vary significantly. As a result, there is a considerable heat transfer variation between the boundary layer and the wall of the hypersonic vehicle.
Amjad A Pasha, Khalid A Juhany
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Experimental study of slender vehicles at hypersonic speeds
, 1996 An experimental investigation of the hypersonic flow over (i) a wing-body configuration, (ii) a hemi-spherically blunted cone-cylinder body and (iii) a one-half- power-law body has been conducted for M,, = 8.2 and Re,, = 9.35x104
Singh, Amarjit
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Some hypersonic intake studies [PDF]
, 2006 A 'two dimensional' air intake comprisipg a wedge followed by an isentropic compression has been tested in the Cranfield Gun Tunnel at Mach 8,2. These tests were performed to investigate qualitatively the intake flow starting process. The effects of cowl
Lanson, F., Stollery, J. L.
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Modeling and Characteristics of ultraviolet radiation from high-speed vehicles
Kongqi donglixue xuebaoThe rapid advancement of near-space hypersonic vehicles, including air-breathing cruise missiles, strategic glide vehicles, hypersonic boost-glide vehicles, and space-to-ground platforms, has created an urgent need for advanced detection technologies and
Xiaoyi Sun, Yu Wang
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The Hypersonic Experiment SHEFEX - Aerotheromdynamic Layout, Vehicle Development and First Flight Results [PDF]
, 2005 The purpose of the SHarp Edge Flight Experiment SHEFEX was the investigation of the aerodynamic behaviour and thermal problems of possible new shapes for future launcher or re-entry vehicles.
Hörschgen, Marcus +4 more
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