Experimental Investigation Of The Effect Of Vertical Tail Size And Length And Of Fuselage Shape And Length On The Static Lateral Stability Characteristics Of A Model With 45 Sweptback Wing And Tail Surfaces
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Measurements of Section Characteristics of a 45 Degree Swept Wing Spanning a Rectangular Low-speed Wind Tunnel as Affected by the Tunnel Walls
Tunnel-wall corrections for the induced upwash velocity for a swept wing completely spanning a rectangular wind tunnel are included in the appendix.
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
language: en
Publisher:
Release Date: 1957