#
Aerofoils
Resource Information
The concept ** Aerofoils** represents the subject, aboutness, idea or notion of resources found in **University of Oklahoma Libraries**.

The Resource
Aerofoils
Resource Information

The concept

**Aerofoils**represents the subject, aboutness, idea or notion of resources found in**University of Oklahoma Libraries**.- Label
- Aerofoils

- Authority link
- http://id.worldcat.org/fast/00798241

- Source
- fast

## Context

Context of Aerofoils#### Subject of

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- Wind-tunnel tests of a blunt-nose aileron with beveled trailing edge on an NACA 66(215)-216 airfoil with several modification of aileron nose and adjacent airfoil contour
- A general representation for axial-flow fans and turbines
- A modification to thin-airfoil-section theory, applicable to arbitrary airfoil sections, to account for the effects of thickness on the lift distribution
- A rapid implicit-explicit solution to the two-dimensional time-dependent incompressible Navier-Stokes equations
- A simplified mathematical model for calculating aerodynamic loading and downwash for midwing wing-fuselage combinations with wings of arbitrary plan form
- A theoretical and experimental study of wind-tunnel-wall effects on oscillating air forces for two-dimensional subsonic compressible flow
- Absolute coefficients and the graphical representation of aerofoil characteristics
- An Integrating manometer for use in wind tunnel pressure distribution measurements
- An analysis of estimated and experimental transonic downwash characteristics as affected by plan form and thickness for wing and wing-fuselage configurations
- An experimental investigation of transonic flow past two-dimensional wedge and circular-arc sections using a Mach-Zehnder interferometer
- Attainable circulation of airfoils in cascade
- Calculation of the aerodynamic loading of flexible wings of arbitrary plan form and stiffness
- Center of pressure coefficients for airfoils at high speeds
- Charts for estimation of the characteristics of a helicopter rotor in forward flight : 1 - Profile drag-lift ratio for untwisted rectangular blades
- Correspondence flows for wings in linearized potential fields at subsonic and supersonic speeds
- Damping-in-roll calculations for slender swept-back wings and slender wing-body combinations
- Determination of mean camber surfaces for wings having uniform chordwise loading and arbitrary spanwise loading in subsonic flow
- Effect of aerofoil aspect ratio on the slope of the lift curve
- Effect of aspect ratio on undamped torsional oscillations of a thin rectangular wing in supersonic flow
- Effect of protruding gasoline tanks upon the characteristics of an airfoil
- Effect of thickness, camber, and thickness distribution on airfoil characteristics at Mach numbers up to 1.0
- Effects of Mach number up to 0.34 and Reynolds number up to 8,000,000 on the maximum lift coefficient of a wing of NACA 66-series airfoil sections
- Effects of compressibility on lift and load characteristics of a tapered wing of NACA 64-210 airfoil sections up to a Mach number of 0.60
- Effects of compressibility on maximum lift coefficients for six propeller airfoils
- Equations and charts for the rapid estimation of hinge-moment and effectiveness parameters for trailing-edge controls having leading and trailing edges swept ahead of the Mach lines
- Estimation of lift and drag of airfoils at near sonic speeds and in the presence of detached shock waves
- Estimation of the damping in roll of rings through the normal flight range of lift coefficient
- Experimental aerodynamic derivatives of a sinusoidally oscillating airfoil in two-dimensional flow
- Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities
- Extension of the theory of oscillating airfoils of finite span in subsonic compressible flow
- Factors affecting the maximum lift-drag ratio at high supersonic speeds
- Flutter at very high speeds
- Formulas and tables of coefficients for numerical differentiation with function values given at unequally spaced points and application to solution of partial differential equations
- Ice prevention on aircraft by means of engine exhaust heat and a technical study of heat transmission from a Clark Y airfoil
- Influence of span and load per square meter on the air forces of the supporting surface
- Influence of the orifice on measured pressures
- Investigation in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps
- Investigation of a simple device for preventing separation due to shock and boundary-layer interaction
- Investigation of spoiler ailerons for use as speed brakes or glide-path controls on two NACA 65-series wings equipped with full-span slotted flaps
- Isolated and cascade airfoils with prescribed velocity distribution
- Jet array impingement with crossflow - correlation of streamwise resolved flow and heat transfer distributions
- Low-speed experimental investigation of a thin, faired, double-wedge airfoil section with nose and trailing-edge flaps
- Measurements in the boundary layer of a yawed wing
- Method for calculating the rolling and yawing moments due to rolling for unswept wings with or without flaps or ailerons by use of nonlinear section lift data
- Note on the Katzmayr effect on airfoil drag
- Note on the accuracy of a method for rapidly calculating the increments in velocity about an airfoil due to angle of attack
- Note on vortices and on their relation to the lift of airfoils
- On the Second-order tunnel-wall-constriction corrections in two-dimensional compressible flow
- Similarity laws for transonic flow about wings of finite span
- Subsonic two-dimensional-flow conditions near an airfoil determined by static pressures measured at the tunnel wall
- Tests in the Variable Density Wind Tunnel to investigate the effects of scale and turbulence on airfoil characteristics
- The N.A.C.A. CYH airfoil section
- The determination of downwash
- The determination of the angles of attack of zero lift and of zero moment, based on Munk's integrals
- The effect of a change in airfoil section on the hinge-moment characteristics of a half-delta tip control with a 60° sweep angle at a Mach number of 6.9
- The effects of sideslip, aspect ratio, and Mach number on the lift and pitching moment of triangular, trapezoidal, and related plan forms in supersonic flow
- The fairing of airfoil contours
- The reversibility theorem for thin airfoils in subsonic and supersonic flow
- The yawing moment, due to sideslip of triangular, trapezoidal, and related plan forms in supersonic flow
- Theoretical and experimental investigation of the effect of tunnel walls on the forces on an oscillating airfoil in two-dimensional subsonic compressible flow
- Theoretical prediction of pressure distributions on nonlifting airfoils at high subsonic speeds
- Theoretical relations between the stability derivatives of a wing in direct and in reverse supersonic flow
- Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds
- Transient aerodynamic behavior of an airfoil due to different arbitrary modes of nonstationary motions in a supersonic flow
- Two-dimensional low-speed cascade investigation of NACA compressor blade sections having a systematic variation in mean-line loading
- Two-dimensional transonic flow past airfoils
- Variation of peak pitching-moment coefficients for six airfoils as affected by compressibility
- Velocity distributions on arbitrary airfoils in closed tunnels by conformal mapping
- Velocity distributions on symmetrical airfoils in closed tunnels by conformal mapping
- Volterra's solution of the wave equation as applied to three-dimensional supersonic airfoil problems
- Wind tunnel investigation of a plain aileron with various trailing-edge modifications on a tapered wing : 1- Aileron with fixed inset tabs
- Wind tunnel investigation of control surface characteristics : 12 - Various cover-plate alinements on the NACA 0015 airfoil with a 30 percent chord flap and large sealed internal balance
- Wind-tunnel investigation at low speed of lateral control characteristics of an untapered 45° sweptback semispan wing of aspect ratio 1.59 equipped with various 25-percent-chord plain ailerons
- Wind-tunnel investigation of ailerons on a low-drag airfoil : 1 - The effect of aileron profile
- Wind-tunnel investigation of ailerons on a low-drag airfoil : 2 - The effect of thickened and beveled trailing edges
- Wind-tunnel investigation of shielded horn balancees and tabs on a 0.7-scale model of XF6F vertical tail surface
- Wind-tunnel investigation of the boundary layer on an NACA 0009 airfoil having 0.25- and 0.50-airfoil chord plain sealed flaps

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