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A comparison of the experimental and theoretical loading over triangular wings at supersonic speeds

Effect of blade-surface finish on performance of a single-stage axial-flow compressor

Design and performance of an experimental axial-discharge mixed-flow compressor II : over-all performance of impeller and supersonic-diffuser combination

Damping in a roll of a missile configuration with a modified triangular wing and a cruciform tail at a Mach number of 1.52

Effects of spanwise thickness variation on the transonic aerodynamic characteristics of wings having 35 degrees of sweepback, aspect ratio 4, and taper ratio 0.60

Effects of spanwise thickness variation on the aerodynamic characteristics of 35 degree and 45 degree sweptback wings of aspect ratio 6: transonic-bump method

Application of Theodorsen's propeller theory to the calculation of the performance of dual-rotating propellers

Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : triangular wing of aspect ratio 2 with NACA 0005-63 thickness distribution, cambered and twisted for a trapezoidal span load distribution

Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds: twisted and cambered triangular wing of aspect ratio 2 with NACA 0003-63 thickness distribution

A semi-empirical method for calculating the pitching moment of bodies of revolution at low Mach numbers

Effects on the Snaking Oscillation of the Bell X-1 Airplane of a Trailing-Edge Bulb on the Rudder

An investigation of convergent-divergent diffusers at Mach number 1.85

Wind-tunnel investigation at Mach numbers of 1.5 and 2.0 of a canard missile configuration

A velocity-correction formula for the calculation of transonic Mach number distributions over diamond-shaped airfoils

Velocity and temperature fields in circular jet expanding from choked nozzle into quiescent air

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


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