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Line-Vortex Theory for Calculation of Supersonic Downwash
Intensity, scale, and spectra of turbulence in mixing region of free subsonic jet
Analysis and Calculation by Integral Methods of Laminar Compressible Boundary-Layer With Heat Transfer and With and Without Pressure Gradient
Nitrited-Steel Piston Rings for Engines of High Specific Power
Effects of Small Angles of Sweep and Moderate Amounts of Dihedral on Stalling and Lateral Characteristics of a Wing-Fuselage Combination Equipped With Partial- and Full-Span Double Slotted Flaps
Direct method of design and stress analysis of rotating disks with temperature gradient
Laminar-boundary-layer oscillations and transition on a flat plate
Appreciation and Prediction of Flying Qualities
Velocity distributions on two-dimensional wing-duct inlets by conformal mapping
Jet-boundary corrections for reflection-plane models in rectangular wind tunnels
Review of Flight Tests of NACA C and D Cowlings on the XP-42 Airplane
Determination of general relations for the behavior of turbulent boundary layers
Formulas for propellers in yaw and charts of the side-force derivative
Analysis of wind-tunnel stability and control tests in terms of flying qualities of full-scale airplanes
A Theoretical Investigation of Hydrodynamic Impact Loads on Scalloped-Bottom Seaplanes and Comparisons With Experiment
Survey of Portions of the Chromium-Cobalt-Nickel-Molybdenum Quaternary System at 1,200 Degrees C
The effect of blade-section thickness ratio on the aerodynamic characteristics of related full-scale propellers at Mach numbers up to 0.65
Lubrication and cooling studies of cylindrical-roller bearings at high speeds
Effect on longitudinal stability and control characteristics of a Boeing B-29 airplane of variations in stick-force and control-rate characteristics obtained through use of a booster in the elevator-control system
Method of analysis for compressible flow through mixed-flow centrifugal impellers of arbitrary design
Frequency Response of Linear Systems From Transient Data
General algebraic method applied to control analysis of complex engine types
Calculation of the lateral control of swept and unswept flexible wings of arbitrary stiffness
An investigation of four wings of square plan form at a Mach number of 6.9 in the Langley 11-inch hypersonic tunnel
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