Method for calculation of transient aeroelastic effects on airplane wings based on Euler equations of flow. Conforming grids facilitate calculations of flows about changing shapes. Capability to compute aeroelastic effects reduces cost of developing aircraft.
Calculation Of Aeroelastic Transients Using Euler Equations
NASA Tech Briefs ; 15 , 5
1991-05-01
Sonstige
Keine Angabe
Englisch
Aeroelastic Calculations for the Hawk Aircraft Using the Euler Equations
Online Contents | 2005
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