Concepedia

Aerothermodynamics and Transition in High-Speed Wind Tunnels at NASA Langley

Annual Review of Fluid Mechanics · 1990 · 135 citations · 4 references

Concepts

Natural SciencesAerospace EngineeringPhysicsAerodynamicsFluid DynamicsFluid MechanicsPlanetary Boundary LayerTurbulenceTurbulent FlowWind-tunnel TestingAerothermodynamicsBoundary Layer Wind Tunnel TestingExperimental Transonic Wind TunnelsTransition DetectionWind TransportWind Tunnel ModelingWind Tunnel Simulation

Abstract

Aerothermodynamics and Transition in High-Speed Wind Tunnels at NASA Langley, Page 1 of 1 < Previous page | Next page > /docserver/preview/fulltext/fluid/22/1/annurev.fl.22.010190.002223-1.gif

References

4

Boundary-layer transition on a cone and flat plate at Mach 3.5

F.-J. Chen, Mujeeb R. Malik, I. E. Beckwith · AIAA Journal · 1989 · 189 citations

Engineering, Aerospace Engineering, Fluid Dynamics +13

Instabilities and transition in the wall boundary layers of low-disturbance supersonic nozzles

F.-J. CHEN, I. E. Beckwith · 1985 · 39 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

A Program for Transition Research

Eli Reshotko · AIAA Journal · 1975 · 39 citations

Natural Sciences, Earth Sciences, Physics +17

Design requirements for the NASA Langley supersonic low-disturbance wind tunnel

I. E. Beckwith, F.-J. CHEN, T. R. Creel · 1986 · 35 citations

Engineering, Aerospace Engineering, Physics +17