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NACA Technical Notes
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A Low-Speed Experimental Investigation of the Effect of a Sandpaper Type of Roughness on Boundary-Layer Transition
Effect of Wall Cooling on Inlet Parameters of a Scoop Operating in a Turbulent Boundary Layer on a Flat or Conical Surface for Mach Numbers 2 to 10
An approximate analytical method for studying entry into planetary atmospheres
Qualitative Simulator Study of Longitudinal Stick Forces and Displacements Desirable During Tracking
Experimental measurements of the effects of airplane motions on wing and tail angles of attack of a swept-wing bomber in rough air
Flight Investigation of Effects of Atmospheric Turbulence and Moderate Maneuvers on Bending and Torsional Moments Encountered by a Helicopter Rotor Blade
Summary of experimental heat-transfer measurements in turbulent flow for a Mach number range from 0.87 to 5.05
Procedure for calculating flutter at high supersonic speed including camber deflections, and comparison with experimental results
A theoretical analysis of the effect of engine angular momentum on longitudinal and directional stability in steady rolling maneuvers
Experimental investigation of axial and normal force characteristics of skewed nozzles
Measurements in a Shock Tube of Heat-Transfer Rates at the Stagnation Point of a 1.0-Inch-Diameter Sphere for Real-Gas Temperatures Up to 7,900 R
An investigation of some phenomena relating to aural detection of airplanes
Effect of the proximity of the wing first-bending frequency and the short-period frequency on the airplane dynamic-response factor
Graphs of reduced variables for computing histories of vaporizing fuel drops, and drop histories under pressure
An experimental investigation of wake effects on hydro-skis
Low tip Mach number stall characteristics and high tip Mach number compressibility effects on a helicopter rotor having an NACA 0009 tip airfoil section
Hydrodynamic Impact Loads of a -20 Degree Dead-Rise Inverted-V Model and Comparisons With Loads of a Flat-Bottom Model
Measurements of Aerodynamic Forces and Moments at Subsonic Speeds on a Simplified T-Tail Oscillating in Yaw About the Fin Midchord
Wind-tunnel investigation of the high-subsonic static longitudinal stability characteristics of several wing-body configurations designed for high lift-drag ratios at a Mach number of 1.4
Flight Investigation of Effects of Retreating-Blade Stall on Bending and Torsional Moments Encountered by a Helicopter Rotor Blade
Tests of Ring-Stiffened Circular Cylinders Subjected to a Transverse Shear Load
Low-speed experimental determination of the effects of leading-edge radius and profile thickness on static and oscillatory lateral stability derivatives for a delta wing with 60 degrees of leading-edge sweep
Flight Measurements of the Vibratory Bending and Torsional Stresses on a Modified Supersonic Propeller for Forward Mach Numbers up to 0.95
Effects of Propeller Position and Overlap on the Slipstream Deflection Characteristics of a Wing-Propeller Configuration Equipped With a Sliding and Fowler Flap
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