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NACA Technical Notes
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The results of wind-tunnel tests to a Mach number of 0.90 of a four-engine, propeller-driven airplane configuration having a wing with 40 degrees of sweepback and an aspect ratio of 10
Supersonic flow past nonlifting bumped and indented bodies of revolution
Some Observations on the Relationship Between Fatigue and Internal Friction
Equations, Tables, and Figures for Use in the Analysis of Helium Flow at Supersonic and Hypersonic Speeds
Procedure for calculating flutter at high supersonic speed including camber deflections, and comparison with experimental results
Experimental investigation of axial and normal force characteristics of skewed nozzles
An investigation of some phenomena relating to aural detection of airplanes
Graphs of reduced variables for computing histories of vaporizing fuel drops, and drop histories under pressure
Measurements of Aerodynamic Forces and Moments at Subsonic Speeds on a Simplified T-Tail Oscillating in Yaw About the Fin Midchord
Tests of Ring-Stiffened Circular Cylinders Subjected to a Transverse Shear Load
Effects of Propeller Position and Overlap on the Slipstream Deflection Characteristics of a Wing-Propeller Configuration Equipped With a Sliding and Fowler Flap
Application of obliquely mounted strain gage to measurement of residual stresses in disks
Water-Impact Theory for Aircraft Equipped With Nontrimming Hydro-Skis Mounted on Shock Struts
Free-Flight Investigation to Determine the Drag of Flat- and Vee- Windshield Canopies on a Parabolic Fuselage With and Without Transonic Indentation Between Mach Numbers of 0.75 and 1.35
Low tire friction and cornering forces on a wet surface
Effects of ground proximity on the thrust of a simple downward-directed jet beneath a flat surface
Investigation of Minimum Drag and Maximum Lift-Drag Ratios of Several Wing-Body Combinations Including a Cambered Triangular Wing at Low Reynolds Numbers and at Supersonic Speeds
An Approach to the Problem of Estimating Severe and Repeated Gust Loads for Missile Operations
Effect of Some External Crosswise Stiffeners on the Heat Transfer and Pressure Distribution on a Flat Plate at Mach Numbers of 0.77, 1.39, and 1.98
Lag in Pressure Systems at Extremely Low Pressures
Hydrodynamic Impact Loads on 30 Degree and 60 Degree V-Step Plan-Form Models With and Without Dead Rise
Effects of Airplane Flexibility on Wing Strains in Rough Air at 5,000 Feet as Determined by Flight Tests of a Large Swept-Wing Airplane
A Thermal System for Continuous Monitoring of Laminar and Turbulent Boundary-Layer Flows During Routine Flight
Impact-Loads Investigation of Chine-Immersed Model Having a Circular-Arc Transverse Shape
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