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Boundary Layer Effects On Unsteady Airloads by North Atlantic Treaty Organization. Advisory Group For Aerospace Research And Development. Structures And Materials Panel.
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1DTIC ADA098057: Boundary Layer Effects On Unsteady Airloads.
By Defense Technical Information Center
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.
“DTIC ADA098057: Boundary Layer Effects On Unsteady Airloads.” Metadata:
- Title: ➤ DTIC ADA098057: Boundary Layer Effects On Unsteady Airloads.
- Author: ➤ Defense Technical Information Center
- Language: English
“DTIC ADA098057: Boundary Layer Effects On Unsteady Airloads.” Subjects and Themes:
- Subjects: ➤ DTIC Archive - ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE) - *SYMPOSIA - *BOUNDARY LAYER - *AERODYNAMIC LOADING - *TRANSONIC FLOW - THICKNESS - EXPERIMENTAL DATA - SHOCK WAVES - TURBULENT FLOW - AEROELASTICITY - MATHEMATICAL PREDICTION - SUBSONIC FLOW - WINGS - NAVIER STOKES EQUATIONS - OSCILLATION - VISCOUS FLOW - FLOW SEPARATION - PRESSURE DISTRIBUTION - REYNOLDS NUMBER - FLUTTER - SUPERCRITICAL AIRFOILS
Edition Identifiers:
- Internet Archive ID: DTIC_ADA098057
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 127.77 Mbs, the file-s for this book were downloaded 73 times, the file-s went public at Wed Dec 13 2017.
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