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- W568512249 abstract "Report presenting an investigation conducted in the 4- by 4-foot supersonic pressure tunnel at Mach number 1.41 and 2.01 to determine the static lateral and directional stability and control characteristics of a scale model of the Republic F-105 airplane. Results regarding the static lateral and directional stability and lateral and directional control are provided." @default.
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- W568512249 date "1956-11-19" @default.
- W568512249 modified "2023-09-24" @default.
- W568512249 title "Static lateral and directional stability and control characteristics of revised 1/22-scale model of the Republic F-105 airplane at Mach numbers of 1.41 and 2.01 : COORD No. AF-163" @default.
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