Passive control of suddenly expanded flow and temperature distribution along the duct at critical Mach number. [PDF]
Tamboli S +8 more
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Ding GH, Ma BH, Deng JJ, Yuan WZ, Liu K.
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Transonic Wind Tunnel Test of Three-dimensional Wing
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Analysis of some interference effects in a transonic wind tunnel
Journal of Aircraft, 1995The effects of the walls of a test section on a model in transonic flow were investigated by using the AGARD Calibration Model B. Tests were carried out in a closed-circuit pressurized tunnel, with a confined square test section of 1.5 m width, with tapered slots giving a 5% porosity. Two models with different dimensions were used, with 0.85 and 0.056%
LOMBARDI, GIOVANNI, Morelli M.
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