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An Investigation of the Influence of Lift on Sonic-boom Intensity by Means of Wind-tunnel Measurements of the Pressure Fields of Several Wing-body Combinations at a Mach Number of 2.01
出版National Aeronautics and Space Administration, 1961
URLhttp://books.google.com.hk/books?id=8YsOzk8HDfIC&hl=&source=gbs_api
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