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National Advisory Committee for Aeronautics Collection
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National Advisory Committee for Aeronautics Collection
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National Advisory Committee for Aeronautics Collection
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Turbulent Skin Friction at High Mach Numbers and Reynolds Numbers
Aerodynamic Characteristics of a 45 Degree Swept Wing Fighter Airplane Model and Aerodynamic Loads on Adjacent Stores and Missiles at Mach Numbers of 1.57, 1.87, 2.16, and 2.53
Aerodynamic Characteristics of a 45 Degree Swept-Wing Fighter-Airplane Model and Aerodynamic Loads on Adjacent Stores and Missiles at Mach Numbers of 1.57, 1.87, 2.16, and 2.53
Aerodynamic characteristics of several jet-spoiler controls on a 45 degree sweptback wing at Mach numbers of 1.61 and 2.01
Calculation of the Lateral Stability of a Directly Coupled Tandem-Towed Fighter Airplane and Correlation with Experimental Data
An Experimental Investigation of the Static Longitudinal Stability and Control Characteristics of a Wingless Missile Configuration at Mach Numbers From 3.0 to 6.3
Some Effects of Mass Ratio on the Transonic Flutter Characteristics of Untapered 45 Degree Sweptback Wings of Aspect Ratios 2 and 3.5
Aerodynamic characteristics of a canard and an outboard-tail airplane model at a Mach number of 2.01
The Effects of Body Vortices and the Wing Shock-Expansion Field on the Pitch-Up Characteristics of Supersonic Airplanes
The Effects of Body Vortices and the Wing Shock-Expansion Field on the Pitch-Up Characteristics of Supersonic Airplanes
Feasibility of Nose-Cone Cooling by the Upstream Ejection of Solid Coolants at the Stagnation Point
Heat Transfer to 0 Degree and 75 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers From 1.90 to 3.07
Preliminary Study of Airplane Configurations Having Tail Surfaces Outboard of the Wing Tips
Behavior of Some Materials and Shapes in Supersonic Free Jets at Stagnation Temperatures Up to 4,210 Degrees F, and Descriptions of the Jets
High-speed landing loads measured on the Douglas X-3 research airplane
An Investigation of Supersonic Store Interference in the Vicinity of a 22 Degree Swept Wing Fuselage Configuration at Mach Numbers of 1.61 and 2.01
An investigation of supersonic store interference in the vicinity of a 22 degree swept-wing-fuselage configuration at Mach numbers of 1.61 and 2.01
Effects of Leading-Edge Slat and Trailing-Edge Split Flap on the Aerodynamic Characteristics of a Wing-Fuselage Combination Having a Nearly Triangular Wing of Aspect Ratio 2.9 at Mach Numbers From 0.60 to 0.92
Free-flight roll performance of a steady-flow jet-spoiler control on an 80 degree delta-wing missile between Mach numbers of 0.6 and 1.8
Transonic Flutter Investigation of Models of the All-Movable Horizontal Tail of a Fighter Airplane
Transonic Flutter Investigation of Models of the All-Movable Horizontal Tail of a Fighter Airplane
Wind-Tunnel Investigation of the Use of Leading-Edge and Trailing-Edge Area-Suction Flaps on a 13-Percent-Thick Straight Wing and Fuselage Model
Blow-Out Velocities of Solutions of Hydrocarbons and Boron Hydride - Hydrocarbon Reaction Products in a 1 7/8-Inch-Diameter Combustor
Heat of Combustion of the Product Formed by the Reaction of Acetylene and Diborane (LFPL-CZ-3)
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