Boundary Layer Effects on Unsteady Airloads.
Abstract
Partial Contents: Prediction Methods and Comparison with Experiments -- Assessment of theoretical models for viscous and transonic flow, Oscillating supercritical airfoils in the transonic regime with viscous interactions, Methodes de calcul des couches limites instationnaires, Viscous effects on unsteady airloads of oscillating configurations, Prise en compte d'effets de couche limite instationnaire dans un calcul bidimensionnel transsonique, Experimental flutter at high subsonic speeds and its theoretical prediction taking into account wing thickness and reynolds number, Analysis of turbulent flow about an isolated airfoiling using a time-dependent Navier-Stokes procedure; Experimental Studies -- Scale effects on oscillating airfoils at transonic speeds, Unsteady airloads on oscillating control surfaces in subsonic flow, Oscillatory flows from shock-induced separations on biconvex aerofoils of varying thickness in ventilated wind tunnels, and Experiments on a turbulent unsteady boundary layer with separation.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 01, 1981
- Accession Number
- ADA098057
Entities
Organizations
- AGARD