NASA  / MEMO 5-20-59L <br/>
Hewes,Donald E <br/>
       LOW-SUBSONIC MEASUREMENTS OF THE STATIC AND OSCILATORY LATERAL STABILITY DERIVATIVES OF A SWEPTBACK-WING AIRPLANE CONFIGURATION AT ANGLES OF ATTACK FROM-10 D/C TO 90 D/C 
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 .-  Nasa, Washington, D.C.,  1959 
<br/>Bound With Nasa Memo 5-12-59l-5-18-59l And 5-23-59l-28 Lack No.14-17, 19, 21-22, And 27 
<br><U>Copy Details:</u><br> Acc. No.: <b>TR7407</b>, Full Call No.: NASA MEMO 5-20-59L,   Item type:  Technical Report , Location: General Stacks, <br><b>------------------------- --------------------- ------ --------- ------- ------- --------- -------- </b><br>