LIFT (Aerodynamics)REYNOLDS numberDRONE aircraftANGLESUnmanned Combat Aerial Vehicles (UCAVs) are designed to be lightweight and compact, which can impact their overall lift and aerodynamic capabilities. This study focuses on enhancing the Coefficient of Lift (CL) by optimising t...
Both have their advantages and disadvantages. Since several wind tunnel models are required to accomplish aerodynamic experiments, nowadays, one of the best methods for models and airfoils manufacturing are...会议名称: Aiaa Applied Aerodynamics Conference 会议时间: 2006 被引量: 31 ...
Daniel T. Valentine, in Aerodynamics for Engineering Students (Seventh Edition), 2017 3.11.2 Shock-Wave/Boundary-Layer Interaction in Supersonic Flow One of the main differences between subsonic and supersonic flows, as far as boundary-layer behavior is concerned, is that the pressure gradient ...
Lambda wingLeading edge vortexTransition SSTPurpose In this paper, experimental and numerical results of a lambda wing have been compared. The purpose of this paper is to study the behaviour of lambda wings using a CFD tool and to consider different numerical models to obtain the most accurate ...
School of Mechanical, Aerospace and Civil Engineering, The University of Manchester, Manchester, M139PL, UK thomas.shearwood@manchester.ac.uk;School of Mechanical, Aerospace and Civil Engineering, The University of Manchester, Manchester, M139PL, UK;School2018 Applied Aerodynamics Conference: Applied ...
An experiment investigating the laminar鈥搕urbulent transition of a Blasius boundary-layer-like flow was set up in the laminar water channel at the Institute of Aerodynamics and Gas Dynamics, University of Stuttgart. The late stage of controlled transition with K-type breakdown was investigated with...
Rein, M., Gardner, A. D., and Rutten, M., "Study of the influence of a highly integrated flow-through intake on compressible flows about the lambda wing configuration SACCON," 30th AIAA Applied Aerodynamics Conference, AIAA-2012-3324, New Orleans, LA, June 2012....
Theoretical or Mathematical/ aerodynamicsaerospace componentsautomotive componentsboundary layer turbulencefinite volume methodstransonic flow/ local mechanical actionheat additionlambda-shaped shockunsteady transonic flowtwo-dimensional airfoilSST turbulence model. The equations are integrated using the finite volume ...
The planform aerodynamics is governed by complex non-linear flow phenomena due to leading edge vortex flow separation at moderate to high angles of attack. Based on the numerical results, an interpretation of the complex vortex flow is given to understand the unsteady flow phenomena for a variety...