Aerodynamic Loads

194 books
Nacelle Aerodynamic and Inertial Loads (NAIL) projectUnknown Author

Nacelle Aerodynamic and Inertial Loads (NAIL) project

Unknown Author

1982No page data
A program for calculating load coefficient matrices utilizing the force summation method, L218 (LOADS)Unknown Author

A program for calculating load coefficient matrices utilizing the force summation method, L218 (LOADS)

Unknown Author

1979No page data
A modified T-value method for selection of strain gages for measuring loads on a low aspect ratio wingMing Han Tang
⏱ 51m

A modified T-value method for selection of strain gages for measuring loads on a low aspect ratio wing

Ming Han Tang

198051 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 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 LoadsWilliam L. Coulbourne

Wind Loads

William L. Coulbourne

2020No page data
Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representationsJacob H. Lichtenstein
⏱ 46m

Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations

Jacob H. Lichtenstein

197846 pp.
Aircraft dynamic loads due to flow separationNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
⏱ 4h 32m

Aircraft dynamic loads due to flow separation

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

1990272 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.
Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representationsJacob H Lichtenstein
⏱ 46m

Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations

Jacob H Lichtenstein

197846 pp.
Design of a 4-1/2 stage turbine with a stage loading factor of 4.66 and high specific work outputP. F. Webster
⏱ 2h 8m

Design of a 4-1/2 stage turbine with a stage loading factor of 4.66 and high specific work output

P. F. Webster

1976128 pp.
PDSS/IMC qualification test, user's manualUnknown Author

PDSS/IMC qualification test, user's manual

Unknown Author

1984No page data
Aerodynamic interference of high speed ground vehiclesG. W. Johnston

Aerodynamic interference of high speed ground vehicles

G. W. Johnston

1974No 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.
Effect of an alternate winglet on the pressure and spanwise load distributions of a first-generation jet transport wingLawrence C. Montoya
⏱ 1h 32m

Effect of an alternate winglet on the pressure and spanwise load distributions of a first-generation jet transport wing

Lawrence C. Montoya

197892 pp.
A summary of the forebody high-angle-of-attack aerodynamics research on the F-18 and the X-29A aircraftLisa J. Bjarke

A summary of the forebody high-angle-of-attack aerodynamics research on the F-18 and the X-29A aircraft

Lisa J. Bjarke

1992No page data
Aircraft loads due to turbulence and their impact on design and certificationNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
⏱ 1h 40m

Aircraft loads due to turbulence and their impact on design and certification

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

1994100 pp.
Improvements to the missile aerodynamic prediction code DEMON3Marnix F. E. Dillenius
⏱ 2h 46m

Improvements to the missile aerodynamic prediction code DEMON3

Marnix F. E. Dillenius

1992166 pp.
Aerodynamic force analysisBranimir D. Djordjevic

Aerodynamic force analysis

Branimir D. Djordjevic

1966No page data
Flight load spectra and strain prediction equations for Ceres aircraftR. S. Trayford
⏱ 12m

Flight load spectra and strain prediction equations for Ceres aircraft

R. S. Trayford

196712 pp.
Sergio Adrián PérezSergio Adrián Pérez

Sergio Adrián Pérez

Sergio Adrián Pérez

1990No page data
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