Robinson, Ross B. <br/>
       NASA Memo [10-2-58L] : AERODYNAMIC CHARACTERISTICS FOR COMBINED ANGLES OF ATTACK AND SIDESLIP OF A LOW-ASPECT-RATIO CRUCIFORM-WING MISSILE CONFIGURATION EMPLOYING VARIOUS CANARD AND TRAILING-EDGE FLAP CONTROLS AT A NO.2.01 
 / Ross B. Robinson and M. Leroy Spearman 
 .- Washington: National Aeronautics and Space Administration,  1958 
 .- 71p. 
.- ( NASA Memorandum   
<br/>NASA Memorandum 10-1-58L-10-17-58L<br/>Bound Vol. No.102461; Contents: TR-8572-8580 
<br/><u>Subject Headings:</u> <br/>Aerodynamics;
<br/><U>Author Added Entry: </u><br/>Spearman, M. Leroy;
<br><U>Copy Details:</u><br> Acc. No.: <b>TR8572</b>, Full Call No.: ,   Item type:  Technical Report , Location: COMPACT STORAGE (BASEMENT), NASA MEMO-10-2-58L<br><b>------------------------- --------------------- ------ --------- ------- ------- --------- -------- </b><br>