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Primary view of Rocket-Model Investigation to Determine the Hinge-Moment and Normal-Force Properties of a Full-Span, Constant-Chord, Partially Balanced Trailing-Edge Control on a 60 Degree Clipped Delta Wing Between Mach Numbers of 0.50 and 1.26
Martz, C. William & Goslee, John W.
October 30, 1953
Primary view of A pressure-distribution investigation of a fineness-ratio-12.2 parabolic body of revolution (NACA RM-10) at M = 1.59 and angles of attack up to 36 degrees
Cooper, Morton; Gapcynski, John P. & Hasel, Lowell E.
October 30, 1952
Primary view of Preliminary investigation of the effects of several seeker-nose configurations on the longitudinal characteristics of a canard-type missile at a Mach number of 1.60
Robins, A. Warner
October 30, 1953
Primary view of Experimental investigation of performance and operating characteristics of a tail-pipe burner for a turbojet engine
Gabriel, David S.; Martinson, E. Vincent & Essig, Robert H.
October 30, 1947
Primary view of Preliminary investigation of the pressure fluctuations in the wakes of two-dimensional wings at low angles of attack
Sorenson, Robert M.; Wyss, John A. & Kyle, James C.
October 30, 1951
Primary view of Thrust Loading of the NACA 3-(3)(05)-05 Eight-Blade Dual-Rotating Propeller as Determined From Wake Surveys
Platt, Robert J., Jr.
October 30, 1952
Primary view of Wake Surveys in the Slipstream of a Full-Scale Supersonic-Type Three-Blade Propeller at Mach Numbers to 0.96
Swihart, John M. & Norton, Harry T., Jr.
October 30, 1953
Primary view of Aerodynamic characteristics in pitch of a series of cruciform-wing missiles with canard controls at a Mach number of 2.01
Spearman, M. Leroy
October 30, 1953
Primary view of Preliminary Tests of a Buffet Stall-Warning Device on a 1/5-Scale Model of the Republic XP-84 Airplane
Tucker, Warren A. & Comisarow, Paul
October 30, 1946
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