Wind-tunnel tests of a full-scale model of the Republic XF-91 airplane were conducted to determine the distribution of pressure over the external wing fuel tank installation and over the vee tail and ventral fin. The data were obtained for a range of angles of attack and sideslip and elerudder deflection angles; the presentation is in tabular form.
An Investigation of a Full-Scale Model of the Republic XF-91 Airplane in the Ames 40- By 80-Foot Wind Tunnel: Pressure Data
1949-03-25
Miscellaneous
No indication
English
Investigation of diving moments of pursuit airplane in Ames 16-foot high-speed wind tunnel
Engineering Index Backfile | 1942
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