Wind-tunnel/flight Correlation Study of Aerodynamic Characteristics of a Large Flexible Supersonic Cruise Airplane CXB-70-1). 1: Wind-tunnel Tests of a 0.03-scale Model at Mach Numbers from 0.6 to 2.53

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1979 - 222 pages

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Contents

Section 1
25
Section 2
28
Section 3
29

46 other sections not shown

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