NASA Memorandum [NASA MEMO 4-21-59A]:  Longitudinal stability and control characteristics at mach numbers from 0.70 to 2.22 of a triangular wing configuration equipped with a canard control, a trailing-edge-flap control or a cambered forebody 
 / John W. Boyd and Gene P. Menees 
 .- Washington: NASA,  1959 
 .- 39p . 
.- ( National Aeronautics and Space Administration NASA Memorandum   
<br/>Bound together NASA MEMO 4-14-59A to 4-27-59A  <br/>Lack No.4-16 to 4-17, 4-22 to 4-25                                       Bound vol. Acc. No. 102439 contains Acc. No. TR11609 to TR11615 
<br/><u>Subject Headings:</u> <br/>Longitudinal control devices --Tests;
<br/><U>Author Added Entry: </u><br/>Boyd, John W.;<br/>Menees, Gene P. ;
<br><U>Copy Details:</u><br> Acc. No.: <b>TR11613</b>, Full Call No.: ,   Item type:  Technical Report , Location: COMPACT STORAGE (BASEMENT), NASA MEMO 4-14-59A to 4-27-59A<br><b>------------------------- --------------------- ------ --------- ------- ------- --------- -------- </b><br>