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- Laminar friction and heat transfer at Mach numbers from 1 to 10
- Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : triangular wing of aspect ratio 4 with NACA 0005-63 thickness distribution, cambered and twisted for trapezoidal span load distribution
- On the angular distribution of slip lines in polycrystalline aluminum alloy
- Compilation and review of effects of design parameters on ditching characteristics
- Investigation at low speed of the effectiveness and hinge moments of a constant-chord elevator on a large-scale triangular wing with section modification
- An investigation at Mach numbers of 1.40 and 1.59 of the effects of aileron profile on the aerodynamic characteristics of a complete model of a supersonic aircraft configuration
- Investigation of dynamic characteristics of a turbine-propeller engine
- The effect of thickness ratio on section thrust distribution as determined from a study of wake surveys of the NACA 4-(0)(03)-045 and 4-(0)(08)-045 two-blade propellers up to forward Mach numbers of 0.925
- Force and pressure characteristics for a series of nose inlets at Mach numbers from 1.59 to 1.99 5: analysis and comparison on basis of ram-jet aircraft range and operational characteristics
- A comparison of the turbulent boundary-layer growth on an unswept and a swept wing
- Theoretical analysis of some simple types of acceleration restrictors
- The effects of boundary-layer control on the longitudinal characteristics of a swept-back wing using suction through streamwise slots in the outboard portion of the wing
- The effects of centrally mounted wing-tip tanks on the subsonic aerodynamic characteristics of a wing of aspect ratio 10 with 35 degrees of sweepback
- The effects of camber and twist on the aerodynamic loading and stalling characteristics of a large-scale 45 degree swept-back wing
- Contributions of wing, tail, and fuselage to the aerodynamic characteristics of a semispan model of a supersonic airplane configuration at transonic speeds from tests by the NACA wing-flow method
- A correlation of experimental zero-lift drag of rectangular wings with symmetrical NACA 65-series airfoil sections by means of the transonic similarity law for wings of finite aspect ratio
- Pressure-distribution measurements over a 45 degree sweptback wing at transonic speeds by the NACA wing-flow method
- Examples of three representative types of airfoil-section stall at low speed
- Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds: Plane triangular wing of aspect ratio 4 with NACA 0005-63 section
- Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : plane triangular wing of aspect ratio 2 with NACA 0005-63 section
- Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds: Plane triangular wing of aspect ratio 2 with NACA 0003-63 section
- An analysis of flow in rotating passage of large radial-inlet centrifugal compressor at tip speed of 700 feet per second
- Preliminary flight investigation of the maneuvering accelerations and buffet boundary of a 35 degree swept-wing airplane at high altitude and transonic speeds
- Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : plane triangular wing of aspect ratio 2 with NACA 0008-63 section
- Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds: Plane triangular wing of aspect ratio 4 with 3-percent-thick rounded nose section
- Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : plane triangular wing of aspect ratio 3 with NACA 0003-63 section
- Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds: Plane triangular wing of aspect ratio 4 with 3-percent-thick, biconvex section
- Theoretical performance of lithium and fluorine as a rocket propellant
- Approximate methods for calculating the flow about nonlifting bodies of revolution at high supersonic airspeeds
- Note on flutter of a 60 degree delta wing encountered at low-supersonic speeds during the flight of a rocket-propelled model
- An investigation of the effect of vertical-fin location and area on low-speed lateral stability derivatives of a semitailless airplane model
- Effect of a deflectable wing-tip control on the low-speed lateral and longitudinal characteristics of a large-scale wing with the leading edge swept back 47.5 degrees
- A method for predicting the upwash angles induced at the propeller plane of a combination of bodies with an upswept wing
- Wing-on and wing-off longitudinal characteristics of an airplane configuration having an thin unswept tapered wing of aspect ratio 3, as obtained from rocket-propelled models at Mach numbers from 0.8 to 1.4
- Investigation of the effects of geometric changes in an underwing pylon suspended external store installation on the aerodynamic characteristics of a 45 degree sweptback wing at high subsonic speeds
- Free-flight measurements at Mach numbers from 0.7 to 1.6 of some effects of airfoil-thickness distribution and trailing-edge angle on aileron rolling effectiveness and drag for wings with 0 and 45 degrees sweepback
- Large-Scale Flight Measurements of Zero-Lift Drag at Mach Numbers from 0.87 to 1.39 of 1/10-Scale Models of the Northrop MX-775A Missile
- Integrals and integral equations in linearized wing theory
- NACA investigation of fuel performance in piston-type engines
- Graphic Analysis of American and British Axial-Flow Turbojet Engine Performance Trends (Current and Future)
- Heat transfer to bodies in a high-speed rarified-gas stream
- A correlation by means of transonic similarity rules of experimentally determined characteristics of a series of symmetrical and cambered wings of rectangular plan form
- Correlation of physical properties with molecular structure for some dicyclic hydrocarbons having high thermal-energy release per unit volume -- 2-alkylbiphenyl and the two isomeric 2-alkylbicyclohexyl series
- Comparison between theory and experiment for wings at supersonic speeds
- Analysis of plane-plastic stress problems with axial symmetry in strain-hardening range
- Behavior of fast moving flow of compressible gas in cylindrical pipe in presence of cooling
- Analysis of means of improving the uncontrolled lateral motions of personal airplanes
- Effect of tunnel configuration and testing technique on cascade performance
- Experimental investigation of the effect of vertical-tail size and length and of fuselage shape and length on the static lateral stability characteristics of a model with 45 degree sweptback wing and tail surfaces
- Systematic Two-Dimensional Cascade Tests of NACA 65-Series Compressor Blades at Low Speeds