Works matching DE "HYPERSONIC wind tunnels"
Results: 17
Experimental investigation of flow past simple model bodies in hypersonic wind tunnels at similar values of the Mach and Reynolds numbers but at different physical flow velocities.
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- Fluid Dynamics, 2015, v. 50, n. 1, p. 109, doi. 10.1134/S0015462815010123
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ANALYSIS OF DIFFUSION WITHIN CAVITY REGION OF POLLUTANTS FROM SHORT-POINT SOURCES -- WIND TUNNEL EXPERIMENTAL INVESTIGATION.
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- Environment Protection Engineering, 2008, v. 34, n. 4, p. 43
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Erbium oxide aerodynamic models in the hypersonic flow.
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- High Temperature, 2012, v. 50, n. 4, p. 512, doi. 10.1134/S0018151X12040013
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Possible uses of optical methods for determining the structure of nonequilibrium hypersonic flows.
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- High Temperature, 2007, v. 45, n. 3, p. 377, doi. 10.1134/S0018151X07030157
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- Article
Visualization of Vortex at Aero-Spike Root Using Hydraulic Analogy.
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- International Review of Aerospace Engineering, 2017, v. 10, n. 4, p. 189, doi. 10.15866/irease.v10i4.12816
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Hypersonic Wind Tunnel Experiments on Icy Body and their Potential Contribution to Astrobiology.
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- International Review of Aerospace Engineering, 2010, v. 3, n. 2, p. 115
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Investigation of Flow Field in a Typical Hypersonic Wind Tunnel over a Standard Mode.
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- Journal of Applied Fluid Mechanics, 2013, v. 6, n. 4, p. 529, doi. 10.36884/jafm.6.04.21442
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Control of stationary cross-flow modes in a Mach 6 boundary layer using patterned roughness.
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- Journal of Fluid Mechanics, 2018, v. 856, p. 822, doi. 10.1017/jfm.2018.636
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Unstart phenomena induced by mass addition and heat release in a model scramjet.
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- Journal of Fluid Mechanics, 2016, v. 797, p. 604, doi. 10.1017/jfm.2016.282
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Starting characteristics of the hypersonic wind tunnel with the mach number variation.
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- Journal of Mechanical Science & Technology, 2014, v. 28, n. 6, p. 2197, doi. 10.1007/s12206-014-0507-6
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Modern developments in hypersonic wind tunnels.
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- Aeronautical Journal, 2006, v. 110, n. 1103, p. 21, doi. 10.1017/S0001924000004346
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Numerical simulation of receptivity of a hypersonic boundary layer to acoustic disturbances.
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- Journal of Applied Mechanics & Technical Physics, 2007, v. 48, n. 3, p. 368, doi. 10.1007/s10808-007-0046-3
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Use of high pressures for solving problems of hypersonic aerodynamics.
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- Journal of Applied Mechanics & Technical Physics, 2000, v. 41, n. 5, p. 855, doi. 10.1007/BF02468731
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Drag reduction on a spiked body at hypersonic speed.
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- Aeronautical Journal, 2010, v. 114, n. 1152, p. 113
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Flow Control by Repetitive Discharge for Space Vehicle at High Altitude.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 27
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Study of Aerodynamic Characteristics Evaluation under Hypersonic Rarefied Flows.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 13
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Application of a Relaxation Method for Real Gas Flow Over a Reentry Configuration.
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- International Journal of Transport Phenomena, 2008, v. 10, n. 2, p. 157
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