1977
DOI: 10.21236/ada038494
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Static Stability and Drag Effects of Various External Store Configurations on the F-15 Aircraft at Mach Numbers from 0.6 to 1.3

Abstract: Approved for public release; dtstrtbution unlimited m =( M ,.I ,.I 4[ _o Z =¢ ..q ~r,-• c i (= m ~m m m

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