Partial Contents: CFD code developments and validations at ONEA for helicopter applications; Inverse Design Method for Wing of Supersonic Transport; Study on Transonic Flutter Characteristics of an Arrow Wing Configuration; Aerodynamic Analysis of Helicopter Rotor by Coupling of CFD and Trim Calculation Advanced Technology Institute of Commuter-helicopter; A Numerical Simulation of Flow around Rotor Blades using Overlapped Grid Advanced Technology Institute of Commuter-helicopter; and Thin Body Treatment on Unstructured, Cartesian Grid.
Proceedings of the NAL Symposium on Aircraft Computation Aerodynamics (15th). Held in Tokyo, Japan on June 12-13, 1997
1998
358 pages
Report
Keine Angabe
Englisch
Aerodynamics , Spacecraft Trajectories & Flight Mechanics , Fluid Mechanics , Computational fluid dynamics , Aircraft structures , Aerodynamic configurations , Meetings , Aeronautical engineering , Numerical flow visualization , Unsteady flow , Gas dynamics , Shock waves , Compressible flow , Turbulent flow , Hypersonic flight , Aerothermodynamics , Boundary layer flow , Aerodynamic heating , Enthalpy , Hypersonic flow , Hypersonic reentry , Reentry vehicles , Multiphase flow , Supersonic flow , Airfoils , Subsonic flow , Flow characteristics , Flow distribution , Conservation laws , Multigrid methods , Grid generation(Mathematics) , Wing body configurations , Turbomachinery , Parallel processing , Wake