Wing Loading

64 books
Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wingThomas A. Byrdsong
⏱ 3h 31m

Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing

Thomas A. Byrdsong

1983211 pp.
Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wingThomas A Byrdsong
⏱ 3h 13m

Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing

Thomas A Byrdsong

1983193 pp.
Effects of winglets on a first-generation jet transport wingRobert R. Meyer
⏱ 56m

Effects of winglets on a first-generation jet transport wing

Robert R. Meyer

198656 pp.
In-flight investigation of shuttle tile pressure orifice installationsTimothy R. Moes
⏱ 33m

In-flight investigation of shuttle tile pressure orifice installations

Timothy R. Moes

199033 pp.
An experimental and theoretical analysis of the aerodynamic characteristics of a biplane-winglet configurationPeter D Gall

An experimental and theoretical analysis of the aerodynamic characteristics of a biplane-winglet configuration

Peter D Gall

1984No page data
In-flight transport performance optimizationGlenn B. Gilyard
⏱ 15m

In-flight transport performance optimization

Glenn B. Gilyard

199715 pp.
Dynamic tests on free-flying models of slender wings subjected to sidegustsWilliam Edrington Gray
⏱ 15m

Dynamic tests on free-flying models of slender wings subjected to sidegusts

William Edrington Gray

196815 pp.
Numerical simulation and comparison of symmetrical/supercritical airfoils for the near tip region of a helicopter in forward flightForooz F. Badavi
⏱ 51m

Numerical simulation and comparison of symmetrical/supercritical airfoils for the near tip region of a helicopter in forward flight

Forooz F. Badavi

198951 pp.
Determination of stores pointing error due to wing flexibility under flight loadWilliam A. Lokos

Determination of stores pointing error due to wing flexibility under flight load

William A. Lokos

1995No page data
Response of the alliance 1 proof-of-concept airplane under gust loadsA. S. Naser

Response of the alliance 1 proof-of-concept airplane under gust loads

A. S. Naser

2001No page data
Active load control during rolling maneuversJessica A. Woods-Vedeler

Active load control during rolling maneuvers

Jessica A. Woods-Vedeler

1994No page data
Wing weight optimization under aeroelastic loads subject to stress constraintsUnknown Author

Wing weight optimization under aeroelastic loads subject to stress constraints

Unknown Author

1997No page data
Fluctuating loads measured on an over-the-wing supersonic jet modelConrad M. Willis
⏱ 38m

Fluctuating loads measured on an over-the-wing supersonic jet model

Conrad M. Willis

197938 pp.
High-lift systems on commercial subsonic airlinersPeter K. C. Rudolph
⏱ 2h 35m

High-lift systems on commercial subsonic airliners

Peter K. C. Rudolph

1996155 pp.
Some exact calculations of the lift and drag produced by a wedge in supersonic flowP. L. Roe
⏱ 17m

Some exact calculations of the lift and drag produced by a wedge in supersonic flow

P. L. Roe

196717 pp.
The estimation of the loading on swept wings with extending chord flaps at subsonic speedsJ. McKie
⏱ 30m

The estimation of the loading on swept wings with extending chord flaps at subsonic speeds

J. McKie

197030 pp.
The calculation of the warp to produce a given load and the pressures due to a given thickness on thin slender wings in supersonic flowJeremy H. B. Smith
⏱ 36m

The calculation of the warp to produce a given load and the pressures due to a given thickness on thin slender wings in supersonic flow

Jeremy H. B. Smith

196736 pp.
The unsteady forces on finite wings in transient motionBarrie Dennis Dore
⏱ 50m

The unsteady forces on finite wings in transient motion

Barrie Dennis Dore

196750 pp.
Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wingThomas A. Byrdsong
⏱ 2h 55m

Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing

Thomas A. Byrdsong

1983175 pp.
Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperatureLawrence R. Reardon
⏱ 35m

Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature

Lawrence R. Reardon

198935 pp.
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