[PDF] 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 06 Full Read

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Language: en
Pages: 50

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

Authors: Robert J. Platt

Categories: Aerodynamic load

Type: BOOK - Published: 1955 - Publisher:

A transonic investigation of the effects of sweepback and thickness ratio on the wing loads of a wing in the presence of a body has been made in the Langley 8-f

Language: en
Pages: 86

Transonic Wind-tunnel Investigation of Aerodynamic-loading Characteristics of a 2-percent-thick Trapezoidal Wing in Combination with Basic and Indented Bodies

Authors: Thomas C. Kelly

Categories: Aerodynamic load

Type: BOOK - Published: 1957 - Publisher:

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Pressure data have been obtained in the Langley 8-foot transonic tunnel at Mach numbers from 0.80 to 1.115 and angles of attack from 0 to 20 degrees for wing-bo