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Primary view of Aerodynamic characteristics at Mach number of 2.01 of two cruciform missile configurations having 70 degree delta wings with length-diameter ratios of 14.8 and 17.7 with several canard controls
Spearman, M. Leroy & Robinson, Ross B.
August 30, 1954
Primary view of Effects of Canopy, Revised Vertical Tail, and a Yaw-Damper Vane on the Aerodynamic Characteristics of a 1/16-Scale Model of the Douglas D-558-II Research Airplane at a Mach Number of 2.01
Robinson, Ross B.
August 30, 1954
Primary view of A Flight Evaluation of the Stability and Control of the X-4 Swept-Wing Semitailless Airplane
Sadoff, Melvin & Crossfield, A. Scott
August 30, 1954
Primary view of Pressure Distributions on Plug- and Semaphore-Type Spoiler Ailerons on a 35 Degree Sweptback Wing of Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Section at High Subsonic Speeds
Hammond, Alexander D. & Hayes, William C., Jr.
August 30, 1954
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