INVESTIGATION AT TRANSONIC SPEEDS OF THE LOADING OVER A 45 DEGREE SWEPTBACK WING HAVING AN ASPECT RATIO OF 3, A TAPER RATIO OF 0.2, AND NACA 65A004 AIRFOIL SECTIONS

By Runckel,Jack F. Nasa, Washington, D.C. 1961 . 93 , Bound With Nasa Tn D-701-11, 713-20

INTERACTION EFFECTS OF A CONTROL JET EXHUSTATION RADIALLY FROM THE NOSE OF A OGIVE-CYLINDER BODY AT TRANSONIC SPEEDS.

By Lee,Edwin E. Nasa, Washington, D.C. 1967 . 30 , Bound With Nasa Tn D-3751,3753-60.