Experimental Investigation Of Pressure Distribution And Static Aerodynamic Characteristics For Three Supersonic Impact Ballistic Reentry Shapes At Mach Number Of 193 255 And 305
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Experimental Investigation of Pressure Distribution and Static Aerodynamic Characteristics for Three Supersonic Impact Ballistic Reentry Shapes at Mach Numbers of 1.93, 2.55, and 3.05
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| Total Pages | : 44 |
| Release | : 1961 |
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Download Experimental Investigation of Pressure Distribution and Static Aerodynamic Characteristics for Three Supersonic Impact Ballistic Reentry Shapes at Mach Numbers of 1.93, 2.55, and 3.05 Book in PDF, Epub and Kindle
