NASA  / TN D-4929 <br/>
Queijo,M J <br/>
       THEORY FOR COMPUTING SPAN LOADS AND STABILITY DERIVATIVES DUE TO SIDESLIP YAWING AND ROLLING FOR WINGS IN SUBSONIC COMPRESSIBLE FLOW 
 / 
 .-  Nasa, Washington, D.C.,  1968 
 .- 76 . 
<br/>Bound With Nasa Tn D-4921-28, 4930. 
<br><U>Copy Details:</u><br> Acc. No.: <b>TR12449</b>, Full Call No.: NASA TN D-4929,   Item type:  Technical Report , Location: General Stacks, <br><b>------------------------- --------------------- ------ --------- ------- ------- --------- -------- </b><br>