Analysis and modeling of flight dynamics at high angles of attack; composite blade models; turn over of light aircraft when landing; computation of elastomer structures; a cryogenic model of the A320 aircraft for the wind tunnel; modeling of an isotropic explosion in a uniform flow; validation of tracer behavior models in a flow by holographic velocimetry; and qualification of the lift system of the NES 200 L surface effect ship are discussed.
Activities Report of the Lille Institute of Fluid Mechanics. Annual Report, 1986
1987
15 pages
Report
No indication
English