AN INEXPENSIVE SUPERSONIC WIND TUNNEL FOR HEAT-TRANSFER MEASUREMENTS. PART 1. APPARATUS, DATA, AND RESULTS FOR A LAMINAR BOUNDARY LAYER BASED ON A SIMPLE ONE-DIMENSIONAL FLOW MODEL
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1953 ◽
Vol 20
(7)
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pp. 505-505
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1980 ◽
Vol 102
(3)
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pp. 360-366
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