NASA  / MEMO 4-4-59L - <br/>
Spearman,M Leroy <br/>
       EFFECTS OF FOREBODY DEFLECTION ON STABILITY AND CONTROL CHARACTERISTICS OF A CANARD AIRPLANE CONFIGURATION WITH A HIGH TRAPEZOIDAL WING AT A MACH NUMBER OF 2.01 
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 .-  Nasa, Washington, D.C.,  1959 
 .- 28 . 
<br/>Bound With Nasa Memo 4-1-59l-4-19-59l 
<br/><U>Author Added Entry: </u><br/>Driver,Cornelius;
<br><U>Copy Details:</u><br> Acc. No.: <b>TR7689</b>, Full Call No.: NASA MEMO 4-4-59L -,   Item type:  Technical Report , Location: General Stacks, <br><b>------------------------- --------------------- ------ --------- ------- ------- --------- -------- </b><br>