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Low-Speed Roll Effectiveness of a Differentially Deflected Horizontal-Tail Surface on a 42 Degree Swept-Wing Model
An Investigation at Low Speed of the Spin Instability of Mortar-Shell Tails
Some Effects of Roll Rate on the Longitudinal Stability Characteristics of a Cruciform Missile Configuration as Determined From Flight Test for a Mach Number Range of 1.1 to 1.8
Factors Affecting Loads at Hypersonic Speeds
An analysis of axial- and centrifugal-flow turbojet-engine performance with variable-area exhaust nozzle
Observations on Bauschinger Effect in Copper and Brass
Supplementary Bibliography of NACA Reports Related to Instrumentation and Research Techniques
Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor tip-speed 2: velocity-diagram study of turbine for engine operation with constant exhaust-nozzle area
Drag of circular cylinders for a wide range of Reynolds numbers and Mach numbers
Tabulated Pressure Coefficients and Aerodynamic Characteristics Measured on the Wing of the Bell X-1 Airplane in an Unaccelerated Stall and in Pull-Ups at Mach Numbers of 0.74, 0.75, 0.94, and 0.97
Low-speed longitudinal and wake air-flow characteristics at a Reynolds number of 5.5 x 10(exp 6) of a circular-arc 52 degrees sweptback wing with a fuselage and a horizontal tail at various vertical positions
Calculation of Aerodynamic Forces on an Inclined Dual-Rotating Propeller
An experimental investigation of the effect of various parameters including tip Mach number on the flutter of some model helicopter rotor blades
Some Effects of Roll Rate on the Longitudinal Stability Characteristics of a Cruciform Missile Configuration as Determined From Flight Test for a Mach Number Range of 1.1. To 1.8
The effect of fluid injection on the compressible turbulent boundary layer : the effect of skin friction of air injected into the boundary layer of a cone at M = 2.7
Static lateral stability and control characteristics of a model of a 45 degree swept-wing fighter airplane with various vertical tails at Mach numbers of 1.41, 1.61, and 2.01
A comparison of carrier approach speeds as determined from flight tests and from pilot-operated simulator studies
Ditching Investigation of a 1/12-Scale Model of the Douglas F4D-1 Airplane, TED No. NACA DE 384
Investigation of the NACA 3-(3)(05)-05 Eight-Blade Dual-Rotating Propeller at Forward Mach Numbers to 0.925
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