NASA  / TN D-3893 <br/>
Young,Clarence P <br/>
       A NUMERICAL METHOD FOR DETERMINING THE AEROELASTIC DIVERGENCE CHARACTERISTICS OF UNGUIDED, SLENDER-BODY, MULTISTAGE LAUNCH VEHICLES 
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 .-  Nasa, Washington, D.C.,  1967 
 .- 47 . 
<br/>Bound With Nasa Tn D-3891, 92 And D-3894-3900 
<br><U>Copy Details:</u><br> Acc. No.: <b>TR10425</b>, Full Call No.: NASA TN D-3893,   Item type:  Technical Report , Location: General Stacks, <br><b>------------------------- --------------------- ------ --------- ------- ------- --------- -------- </b><br>