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Use of a scale model in the design of modifications to the NASA Glenn Icing Research Tunnel
Victor A. Canacci2001
Género: Subsonic wind tunnels
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The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel
Norbert Ulbrich
1998
AñadirSubsonic aerodynamic assessment of vortex flow management devices on a high-speed civil transport configuration
Bryan A. Campbell
1999
AñadirEffect of collector configuration on test section turbulence levels in an open-jet wind tunnel
Gregory S. Manuel
1992
AñadirModification of the Ames 40- by 80-foot wind tunnel for component acoustic testing for the second generation supersonic transport
Fredric H. Schmitz
1994
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