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National Advisory Committee for Aeronautics Collection
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The Buckling of Parallel Simply Supported Tension and Compression Members Connected by Elastic Deflectional Springs
Effects of Partial Admission on Performance of a Gas Turbine
Method for Evaluating From Shadow or Schlieren Photographs the Pressure Drag in Two-Dimensional or Axially Symmetrical Flow Phenomena With Detached Shock
The application of airfoil studies to helicopter rotor design
A study of flow changes associated with airfoil section drag rise at supercritical speeds
Effects of Several Design Variables on Turbine-Wheel Weight
On Compressibility Corrections for Subsonic Flow Over Bodies of Revolution
Triangular wings cambered and twisted to support specified distributions of lift at supersonic speeds
The Response of Pressure Measuring Systems to Oscillating Pressures
Equilibrium Operating Performance of Axial-Flow Turbojet Engines by Means of Idealized Analysis
Determination of Rate, Area, and Distribution of Impingement of Waterdrops on Various Airfoils From Trajectories Obtained on the Differential Analyzer
Determination of plate compressive strengths at elevated temperatures
Elastic and plastic buckling of simply supported metalite type sandwich plates in compression
The Longitudinal Stability of Elastic Swept Wings at Supersonic Speed
The Method of Characteristics for the Determination of Supersonic Flow Over Bodies of Revolution at Small Angles of Attack
Laminar mixing of a compressible fluid
Investigation of Icing Characteristics of Typical Light Airplane Engine Induction Systems
Office of Naval Research and NACA Metallurgical Investigation of a Large Forged Disc of S-816 Alloy
NACA and Office of Naval Research Metallurgical Investigation of Two Large Forged Discs of S-590 Alloy
Observations on the Maximum Average Stress of Flat Plates Buckled in Edge Compression
Overbalancing in residual-liquidation computations
Determination of rate, area, and distribution of impingement of of waterdrops on various airfoils from trajectories obtained on the differential analyzer
Aerodynamic characteristics of a flying-boat hull having a length-beam ratio of 15 and a warped forebody
Determination of rate, area, and distribution of impingement of water drops on various airfoils from trajectories obtained on the differential analyzer
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