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NACA Wartime Reports
104
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NACA Wartime Reports
104
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Variation with Mach Number of Static and Total Pressures Through Various Screens
Tests of a 1/14-Scale Powered Model of the XB-36 Airplane in the Langley 19-Foot Pressure Tunnel 1: Stalling Characteristics and Aileron Effectiveness of Several Wing and Flap Arrangements
The Effect of Compression Ratio on Knock Limits of High-Performance Fuels in a CFR Engine 3: Blends of 2,3-Dimethylpentane With 28-R
A theoretical analysis of the effect of aileron inertia and hinge moment on the maximum rolling acceleration of airplanes in abrupt aileron rolls
Variation of Hydrodynamic Impact Loads With Flight-Path Angle for a Prismatic Float at 3 Degree Trim and With a 22 1/2 Degree Angle of Dead Rise
Variation of Hydrodynamic Impact Loads With Flight-Path Angle for a Prismatic Float at 12 Degree Trim and With a 22-1/2 Degree Angle of Dead Rise
Variation of Hydrodynamic Impact Loads With Flight-Path Angle for a Prismatic Float at 6 Degrees and 9 Degrees Trim and a 22-1/2 Degree Angle of Dead Rise
High-speed wind-tunnel tests of the NACA 23012 and 23012-64 airfoils
The Effects of Angle of Dead Rise and Angle of Afterbody Keel on the Resistance of a Model of a Flying-Boat Hull
Knock-limited performance of several internal coolants
The influence of vertical-tail design and direction of propeller rotation on trim characteristics of a twin-engine-airplane model with one engine inoperative
Landing Characteristics of a Model of a Flying Boat With the Depth of Step Reduced to Zero by Means of a Retractable Planing Flap
Improving engine cooling with special baffles
Wind-tunnel tests of a blunt-nose aileron with beveled trailing edge on an NACA 66(215)-216 airfoil with several modifications of aileron nose and adjacent airfoil contour
The Determination of Span Load Distribution at High Speeds by Use of High-Speed Wind-Tunnel Section Data
Progress Summary Number 1: Mechanical Properties of Flush-Riveted Joints Submitted by Five Airplane Manufacturers
Knock-Limited Performance of N-Methylaniline and Xylidine Blends in an Air-Cooled Aircraft Cylinder
Dilution of Exhaust-Gas Samples From a Multicylinder Engine Equipped With an Exhaust-Gas Collector
Determination of the Stability and Control Characteristics of a Tailless All-Wing Airplane Model with Sweepback in the Langley Free-Flight Tunnel
Strain Measurements and Strength Tests on the Tension Side of a Box Beam With Flat Cover
Small-orifice tubes for minimizing dilution in exhaust-gas samples
The belt method for measuring pressure distribution
Considerations of wake-excited vibratory stress in a pusher propeller
Comparison of calculated and experimental propeller characteristics for four-, six-, and eight-blade single-rotating propellers
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