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

The Resource
Aerodynamic load
Resource Information

The concept

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

- Authority link
- http://id.worldcat.org/fast/00798180

- Source
- fast

## Context

Context of Aerodynamic load#### Subject of

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- Wind-tunnel investigation of the effects of steady rolling on the aerodynamic loading characteristics of a 45° sweptback wing at high subsonic speeds
- A Method for determining the aerodynamic characteristics of two- and three-dimensional shapes at hypersonic speeds
- A comparison of the experimental subsonic pressure distributions about several bodies of revolution with pressure distributions computed by means of the linearized theory
- A modification to thin-airfoil-section theory, applicable to arbitrary airfoil sections, to account for the effects of thickness on the lift distribution
- A pressure-distribution investigation of a fineness-ratio-12.2 parabolic body of revolution (NACA RM-10) at M : 1.59 and angles of attack up to 36°
- A study of means for rationalizing airplane design loads
- Aerodynamic characteristics of a leading-edge slat on a 35 degree swept-back wing for Mach numbers from 0.30 to 0.88
- Aerodynamic loading characteristics in sideslip of a 45° sweptback wing with and without a fence at high subsonic speeds
- An analysis of the pressure distribution measured on a body of revolution at transonic speeds in the slotted test section of the Langley 8-foot transonic tunnel
- An experimental investigation of transonic flow past two-dimensional wedge and circular-arc sections using a Mach-Zehnder interferometer
- An experimental study of five annular air inlet configurations at subsonic and transonic speeds
- An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and a 40° sweepback : pressure distribution measurements of the interference effect of the wing on the fuselage at Mach numbers of 1.40 and 1.59
- An investigation of several NACA 1-series nose inlets with and without protruding central bodies at high-subsonic Mach numbers and at a Mach number of 1.2
- Calculation of the aerodynamic loading of flexible wings of arbitrary plan form and stiffness
- Center of pressure coefficients for airfoils at high speeds
- Characteristics of loads in rough air at transonic speeds of rocket-powered models of a canard and a conventional-tail configuration
- Charts and approximate formulas for the estimation of aeroelastic effects on the loading of swept and unswept wings
- Chordwise and compressibility corrections to slender-wing theory
- Comparison of NACA 65-series compressor-blade pressure distributions and performance in a rotor and in cascade
- Determination of mean camber surfaces for wings having uniform chordwise loading and arbitrary spanwise loading in subsonic flow
- Effect of propeller-axis angle of attack on thrust distribution over the propeller disk in relation to wake-survey measurement of thrust
- Effect of thickness, camber, and thickness distribution on airfoil characteristics at Mach numbers up to 1.0
- Effects of compressibility on maximum lift coefficients for six propeller airfoils
- Experimental pressure distributions and force coefficients on block forms for varying Mach number, Reynolds number, and yaw angle
- Experimental pressure distributions over wing tips at Mach number 1.9, [Part] 2, Wing tip with subsonic trailing edge
- Experiments with fabrics for covering airplane wings, to determine effect of method of installation
- Flight investigation at Mach numbers from 0.6 to 1.7 to determine drag and base pressures on a blunt-trailing-edge airfoil and drag of diamond and circular-arc airfoils at zero lift
- Initial experimental investigation of the aerodynamic load on the wing of a model caused by a blast-induced gust that increases the angle of attack into the stall region
- Investigation at Mach numbers from 0.80 to 1.43 of pressure and load distributions over a thin 45° sweptback highly tapered wing in combination with basic and indented bodies
- Investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections
- Lift, pitching moment, and span load characteristics of wings at low speed as affected by variations of sweep and aspect ratio
- Linearized lifting-surface theory for swept-back wings with slender plan forms
- Load distributions associated with controls at supersonic speeds
- Loads associated with spoilers at supersonic speeds
- Loads on wings due to spoilers at subsonic and transonic speeds
- Longitudinal stability characteristics at transonic speeds of a rocket-propelled model of an airplane having a 45 degree swept wing of aspect ratio 6.0
- Measurement and analysis of wing and tail buffeting loads on a fighter-type airplane
- Measurements of fluctuating pressures on the wing of a sweptback wind-body combination in the Langley 16-foot transonic tunnel
- Normal component of induced velocity in the vicinity of a lifting rotor with a nonuniform disk loading
- Note on the pressure distribution over the hull of elongated airships with circular cross section
- On the distribution of lift along the span of an airfoil with displaced ailerons
- Preliminary results of supersonic-jet tests of simplified wing structures
- Pressure distribution and some effects of viscosity on slender inclined bodies of revolution
- Pressure distributions on sphere cones
- Pressure measurements on a body of revolution in the Langley 16-foot transonic tunnel and a comparison with free-fall data
- Remarks on the pressure distributions over the surface of an ellipsoid, moving translationally through a perfect fluid
- Some measurements at subsonic speeds of the aerodynamic forces and moments on two delta wings of aspect ratios 2 and 4 oscillating about the midchord
- Some measurements of aerodynamic forces and moments at subsonic speeds on a rectangular wing of aspect ratio 2 oscillating about the midchord
- Some notes on the aerodynamic loads associated with external-store installations
- Some tables of the factor of apparent additional mass
- Span loadings due to wing twist at transonic and supersonic speeds
- Steady loads due to jet interference on wings, tails, and fuselages at transonic speeds
- Surface pressure distributions on a large-scale 49° sweptback wing-body-tail configuration with blowing applied over the flaps and wing leading edge
- Test of NACA 66,2-116, a : 0.6 airfoil section fitted with pressure balanced and slotted flaps for the wing of the XP-63 airplane
- Tests of four models representing intermediate sections of the XB-33 airplane including sections with slotted flap and ailerons
- The effects of wing incidence on the aerodynamic loading characteristics of a sweptback wing-body combination at transonic speeds
- The proper combination of lift loadings for least drag on a supersonic wing
- Theoretical antisymmetric span loading for wings of arbitrary plan form at subsonic speeds
- Theoretical loading at supersonic speeds of flat swept-back wings with interacting trailing and leading edges
- Theoretical prediction of pressure distributions on nonlifting airfoils at high subsonic speeds
- Theoretical span load distributions and rolling moments for sideslipping wings of arbitrary plan form in incompressible flow
- Transonic wind-tunnel investigation of the effects of sweepback and thickness ratio on the wing loads of a wing-body combination of aspect ratio 4 and taper ratio 0.6
- Variation of peak pitching-moment coefficients for six airfoils as affected by compressibility

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