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- Data presentation of force characteristics of several engine-strut-body configurations at Mach numbers of 1.8 and 2.0 / Robert T. Madden and Emil J. Kremzier
- Effects of altitude on turbojet engine performance
- Base pressures measured on several parabolic-arc bodies of revolution in free flight at Mach numbers from 0.8 to 1.4 and at large Reynolds numbers
- Basic pressure measurements on a fuselage and a 45 degrees sweptback wing-fuselage combination at transonic speeds in the slotted test section of the Langley 8-foot high-speed tunnel
- Aerodynamic characteristics of the NACA RM-10 research missile in the Ames 1- by 3-foot supersonic wind tunnel no. 2: Pressure and force measurements at Mach numbers of 1.52 and 1.98
- Wind-tunnel tests of a 1/12-scale model of the X-3 airplane at subsonic and supersonic speeds.
- Comparison of drag, pressure recovery, and surface pressure of a scoop-type inlet and an NACA submerged inlet at transonic speeds
- A specially constructed metallograph for use at elevated temperatures
- Relation of engine turbine-blade life to stress-rupture properties of the alloys, Stellite 21, Hastelloy B, Cast S-816, Forged S-816, X-40, Nimonic 80, Refractory 26, N-155, and Iconel X
- A recurrence matrix solution for the dynamic response of aircraft in gusts
- Investigation of the liquid fluorine-liquid diborane propellant combination in a 100-pound-thrust rocket engine
- Buckling of thin-walled cylinder under axial compression and internal pressure
- Variation of the pressure limits of flame propagation with tube diameter for propane-air mixtures
- Vaporization rates and heat-transfer coefficients for pure liquid drops
- Experimental investigation of typical constant- and variable-area exhaust nozzles and effects on axial-flow turbojet-engine performance
- The effects at transonic speeds of thickening the trailing edge of a wing with a 4-percent-thick circular-arc airfoil
- An investigation of the control-surface flutter derivatives of an NACA 65(sub 1)-213 airfoil in the Ames 16-foot high-speed wind tunnel
- Direct-reading design charts for 75S-T6 aluminum-alloy flat compression panels having longitudinal extruded Z-section stiffeners
- Experimental investigation of turbojet-engine thrust augmentation by combined compressor coolant injection and tail-pipe burning
- The effects on the aerodynamic characteristics of reversing the wing of a triangular wing-body combination at transonic speeds as determined by the NACA wing-flow method
- Comparison of airfoil sections on two triangular-wing-fuselage configurations at transonic speeds from tests by the NACA wing-flow method
- Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds: Body of revolution
- A Simplified Instrument for Recording and Indicating Frequency and Intensity of Icing Conditions Encountered in Flight
- Calculated Performance of a Direct-Air Nuclear Turbojet-Powered Airplane Using a Split-Flow Reactor and a Separated-Type Shield
- A Summary of Meteorological Conditions Associated With Aircraft Icing and a Proposed Method of Selecting Design Criterions for Ice-Protection Equipment
- Study of Chromium-Frit-Type Coatings for High-Temperature Protection of Molybdenum
- Comparison of Heat Transfer from Airfoil in Natural and Simulated Icing Conditions
- Investigation at Low Speed of 45 Degrees and 60 Degrees Sweptback, Tapered, Low-Drag Wings Equipped With Various Types of Full-Span, Trailing-Edge Flaps
- Skin Friction of Incompressible Turbulent Boundary Layer Under Adverse Pressure Gradients
- Transformations of the Hodograph Flow Equation and the Introduction of Two Generalized Potential Functions
- Relative Structural Efficiencies of Flat Balsa-Core Sandwich and Stiffened-Panel Construction
- Wing-Tunnel Investigation of Effects of Various Aerodynamic Balance Shapes and Sweepback on Control-Surface Characteristics of Semispan Tail Surfaces With NACA 0009, 0015, 66-009, 66(215)-014, and Circular-Arc Airfoil Sections
- Width of Debye-Scherrer Lines for Finite Spectral Width of Primary Beam
- Axial-Momentum Theory for Propellers in Compressible Flow
- Calculation of Higher Approximations for Two-Dimensional Compressible Flow by a Simplified Iteration Process
- A Survey of Creep in Metals
- A Survey of Methods for Determining Stability Parameters of an Airplane From Dynamic Flight Measurements
- The Linearized Characteristics Method and Its Application to Practical Nonlinear Supersonic Problems
- Experimental Investigations of Rolling Performance of Straight and Sweptback Flexible Wings With Various Ailerons
- A General Through-Flow Theory of Fluid Flow With Subsonic or Supersonic Velocity in Turbomachines of Arbitrary Hub and Casing Shapes
- Rotogenerative Detection of Corrosion Currents
- Construction and Use of Charts in Design Studies of Gas Turbines
- A Theory of Conductivity of Cold-Worked Copper
- Theoretical and Experimental Investigation of Condensation of Air in Hypersonic Wind Tunnels
- Method for Analyzing Indeterminate Structures Stressed Above Proportional Limit
- Numerical Determination of Indicial Lift of a Two-Dimensional Sinking Airfoil at Subsonic Mach Numbers From Oscillatory Lift Coefficients With Calculations for Mach Number 0.7
- Approximate Calculation of Turbulent Boundary-Layer Development in Compressible Flow
- Rectangular-Wind-Tunnel Blocking Corrections Using the Velocity-Ratio Method
- Viscosities of Air and Nitrogen at Low Pressures
- On the Application of Mathieu Functions in the Theory of Subsonic Compressible Flow Past Oscillating Airfoils