In this paper, the integration of wind tunnel and flight test procedures are studied for specifying aerodynamic model forms. A procedure is described which employs a stepwise regression method to systematically determine model structures and F-ratio statistics to rank the importance of each aerodynamic coefficient within a given model. Application of this technique and wind tunnel procedures to an oblique-wing aircraft indicate that the aircraft's measured and estimated response are in good agreement at both small and large wing skew angles
Determination of an oblique wing aircraft's aerodynamic characteristics
Atmospheric Flight Mechanics Conference ; 1980 ; Danvers, MA
01.01.1980
Sonstige
Keine Angabe
Englisch
Reliability analysis for a hypersonic aircraft’s wing spar
Emerald Group Publishing | 2019
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