Pages that link to "Item:Q1076570"
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The following pages link to Transonic flow calculations for rigid and flexible wings using a higher- order approximation method (Q1076570):
Displaying 5 items.
- Simplified transonic integral equations for lifting profiles and wings (Q802407) (← links)
- Computation of the Flutter Boundary of the NLR 7301 Airfoil in the Transonic Range (Q3196488) (← links)
- TRANSONIC OBLIQUE-WING FLOW COMPUTATION (Q3694879) (← links)
- (Q4316665) (← links)
- Capturing transition features around a wing by reduced-order modeling based on compressible Navier–Stokes equations (Q5304809) (← links)