CONTROL OF REYNOLDS NUMBER IN A HIGH SPEED WIND TUNNEL. doi: 10.5028/jatm.2009.01016977
Journal of Aerospace Technology and Management, 2011 A conceptual control model for the Reynolds number test based on isentropic relations was established for the supersonic wind tunnel. Comparison of the system response of the model simulation and the actual wind tunnel test data was made to design the ...
Maurício G. Silva +2 more
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The effects of wall surface defects on boundary-layer transition in quiet and noisy supersonic flow [PDF]
The design of supersonic vehicles with laminar flow control and vehicles such as the Space Shuttle requires information on allowable transition tolerances to fabrication defects such as discrete surface roughness and waviness.
Creel, Theodore R., Jr. +1 more
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Wind-tunnel/flight correlation study of aerodynamic characteristics of a large flexible supersonic cruise airplane (XB-701) 2: Extrapolation of wind-tunnel data to full-scale conditions [PDF]
The results of calculations necessary to extrapolate performance data on an XB-70-1 wind tunnel model to full scale at Mach numbers from 0.76 to 2.53 are presented.
Fuller, D. E. +4 more
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Design of a Supersonic Wind Tunnel
, 2011 This study was a preliminary work of how to implement a rocket with sensors in order to get information about the flight.
Torunogullari, Altay +3 more
openaire +1 more source
Hangkong gongcheng jinzhanRotating nozzle profile enables the supersonic variable Mach number wind tunnel to continuously adjust the Mach number of the experimental area during a single operation，which is important for studying the aerodynam ic problems in the maneuvering process
HUANG Kaiyou +4 more
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Experimental study of laminar separation phenomenon combining with numerical calculations
Vietnam Journal of Mechanics, 2011 The separation is much more sensitive for laminar flow than for turbulent flow. These remarks have been attested for both subsonic and supersonic flows.
Nguyen Manh Hung, Hoang Thi Bich Ngoc
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Structure and utilization of supersonic free jets in low density wind tunnels [PDF]
Inviscid and slightly viscous flow in supersonic free jet core, and low density wind tunnel ...
Ashkenas, H., Sherman, F. S.
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Xibei Gongye Daxue XuebaoThe 2 meter high-speed free jet wind tunnel is the first large-scale open jet wind tunnel with Mach number covering sub-span and super-span flow in China.
LIU Weijie +4 more
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Instantaneous Ablation Behavior of Laminated CFRP by High-Power Continuous-Wave Laser Irradiation in Supersonic Wind Tunnel. [PDF]
Materials (Basel), 2023 Ma T, Wang J, Song H, Wang R, Yuan W.
europepmc +1 more source
Space shuttle: Supersonic aerodynamic characteristics of the MSC 040A orbiter (M equals 2.0 to 4.0) [PDF]
A wind tunnel test of the space shuttle orbiter configuration 040A was run in a 20 in. supersonic wind tunnel.
Moore, R. +4 more
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