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National Advisory Committee for Aeronautics Collection
215
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National Advisory Committee for Aeronautics Collection
215
Technical Report Archive and Image Library
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NACA Research Memorandums
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National Advisory Committee for Aeronautics Collection
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Cascade Investigation of Cooling Characteristics of a Castfinned Air-Cooled Turbine Blade for Use in a Turboprop Engine
Summary of Subsonic-Diffuser Data
Wind-Tunnel Investigation at Subsonic and Supersonic Speeds of a Model of a Tailless Fighter Airplane Employing a Low-Aspect-Ratio Swept-Back Wing-Stability and Control
Free-flight Tests of 45 Deg Swept Wings of Aspect Ratio 3.15 and Taper Ratio 0.54 to Measure Wing Damping of the First Bending Mode and to Investigate the Possibility of Flutter at Transonic Speeds
Natural Icing of an Axial-Flow Turbojet Engine in Flight for a Single Icing Condition
Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine. 7: Rotor-Blade Fabrication Procedures
A Method for Calculating the Lift and Center of Pressure of Wing-Body-Tail Combinations at Subsonic, Transonic, and Supersonic Speeds
Rocket-Powered-Model Investigation of the Effects of Aeroelasticity on the Rolling Effectiveness of an 8.06-Percent-Scale McDonnell F3H-1 Airplane Wing at Mach Numbers From 0.5 to 1.4
A Review of NACA Research Through 1954 on Boron Compounds as Fuels for Jet Aircraft (Project Zip)
Local Heat Transfer to Blunt Noses at High Supersonic Speeds
Effect of Several Jet-Engine Air-Inlet Configurations on the Low-Speed Static Longitudinal Stability Characteristics and Quantity Flow of a 1/6-Scale Model of the MX-1764 Airplane
High Mach Number, Low-Cowl-Drag, External-Compression Inlet With Subsonic Dump Diffuser
An Acceleration Schedule Control for Accelerating a Turbojet Engine and Its Use With a Speed Control
Some Factors Affecting the Static Longitudinal and Directional Stability Characteristics of Supersonic Aircraft Configurations
In-Flight Gains Realized by Modifying a Twin Side-Inlet Induction System
Total-Pressure-Recovery Characteristics of a Model of the McDonnell XF3H-1 Inlets and Forebody in a Free Jet at a Mach Number of 1.55
Effects of Some Configuration Changes on Afterburner Combustion Performance
Preliminary Investigation of a Ceramic Lining for a Combustion Chamber for Gas-Turbine Use
Preliminary investigation of spoiler lateral control on a 42 degree sweptback wing at transonic speeds
Full-Scale Investigation of the Maximum Lift and Flow Characteristics of an Airplane Having Approximately Triangular Plan Form
Flight Investigation to Determine the Hinge Moments of a Beveled-Edge Aileron on a 45 Degree Sweptback Wing at Transonic and Low Supersonic Speeds
Two-dimensional wind-tunnel investigation at high Reynolds numbers of two symmetrical circular-arc airfoil sections with high-lift devices
Preliminary Investigation of Two Full-Scale Propellers to Determine the Effect of Swept-Back Blade Tips on Propeller Aerodynamic Characteristics
High-Speed Aerodynamic Characteristics of a Model Tail Plane with Modified NACA 65-010 Sections and 0 Degree and 45 Degrees Sweepback
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