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- Cylinder-head temperatures and coolant heat rejection of a multicylinder liquid-cooled engine of 1650-cubic-inch displacement
- Comparison of theoretical and experimental heat transfer on a cooled 20 degrees cone with a laminar boundary layer at a Mach number of 2.02
- A comparison of theoretical and experimental wing bending moments during seaplane landings
- Effect of an unswept wing on the contribution of unswept-tail configuration to the low-speed static and rolling-stability derivatives of a midwing airplane model
- Effect of aspect ratio on the air forces and moments of harmonically oscillating thin rectangular wings in supersonic potential flow
- The development and performance of two small tunnels capable of intermittent operation at Mach numbers between 0.4 and 4.0
- Investigation of spark-over voltage - density relation for gas-temperature sensing
- Application of the wire-mesh plotting device to incompressible cascade flows
- Relation Between Inflammables and Ignition Sources in Aircraft Environments
- A flight investigation and analysis of the lateral-oscillation characteristics of an airplane
- Stress and distortion measurements in a 45 degree swept box beam subjected to antisymmetrical bending and torsion
- Stress and strain concentration at a circular hole in an infinite plate
- Spectrums and diffusion in a round turbulent jet
- Spin-tunnel investigation to determine the effect on spin recoveries of reducing the opening shock load of spin-recovery parachutes
- The calculation of downwash behind wings of arbitrary plan form at supersonic speeds
- The calculation of modes and frequencies of a modified structure from those of the unmodified structure
- Theoretical analysis of various thrust-augmentation cycles for turbojet engines
- Density fields around a sphere at Mach numbers 1.30 and 1.62
- Maximum pitching angular accelerations of airplanes measured in flight
- Gust-tunnel investigation of a wing model with semichord line swept back 60 degrees
- Charts of thermodynamic properties of air and combustion products from 300 degrees to 3500 degrees R
- The dynamic lateral control characteristics of airplane models having unswept wings with round-and sharp-leading-edge sections
- Graphical method for obtaining flow field in two-dimensional supersonic stream to which heat is added
- The effects of amount and type of camber on the variation with Mach number of the aerodynamic characteristics of a 10-percent-thick NACA 64A- series airfoil section
- Properties of a boron carbide-iron ceramal
- Sintering mechanism between zirconium carbide and columbium
- Laminar-boundary-layer heat-transfer characteristics of a body with a pressure gradient at supersonic speeds
- General method for computation of equilibrium composition and temperature of chemical reactions
- Tables of thermodynamic functions for analysis of aircraft-propulsion systems
- Boundary-layer measurements in 3.84- by 10-inch supersonic channel
- Theoretical turbojet thrust augmentation by evaporation of water during compression as determined by use of a Mollier diagram
- Method for determining optimum division of power between jet and propeller for maximum thrust power of a turbine-propeller engine
- A survey of the flow at the plane of the propeller of a twin-engine airplane
- Investigation of flap-type ailerons on an untapered wing having an aspect ratio of 3.7, 45 degree sweepback, and an NACA 65A009 airfoil section : transonic-bump method
- Flight determination of the effects of rudder-pedal-force characteristics on the aiming error in azimuth of a conventional fighter airplane
- Initial flight investigation of a twin engine supersonic ram jet
- Fundamental flame velocities of pure hydrocarbons 2: alkadienes
- Fundamental flame velocities of pure hydrocarbons 1: alkanes, alkenes, alkynes benzene, and cyclohexane
- High-speed aerodynamic characteristics of a lateral-control model 3: section characteristics, fence studies, and tabulated pressure coefficients with modified NACA 0012-64 section, 26.6-percent-chord, plain aileron, 0 and 45 degree sweepback
- Investigation of perforated convergent-divergent diffusers with initial boundary layer
- An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degree sweepback: Static longitudinal stability and control characteristics at a Mach number of 1.59
- An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degree sweepback : a pressure-distribution study of the aerodynamic characteristics of the wing at Mach number 1.59
- An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degree sweepback
- An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degree sweepback : static lateral stability characteristics at Mach numbers of 1.40 and 1.59
- Investigation of a 1/5-scale model of a proposed high-submerged-speed submarine in the Langley full-scale tunnel
- Investigation of ignition characteristics of AN-F-32 and two AN-F-58a fuels in single can-type turbojet combustor
- The transonic characteristics of a low-aspect-ratio triangular wing with a constant-chord flap as determined by wing-flow tests, including correlation with large-scale tests
- Tests of a small-scale NACA submerged inlet at transonic Mach numbers
- Influence of tube-entrance configuration on average heat-transfer coefficients and friction factors for air flowing in an Inconel tube
- Investigation of stage performance of X24C-2 ten-stage axial-flow compressor at design speed