Accession Number N86-11209/1
Title Airflow Calibration of a Bellmouth Inlet for Measurement of Compressor Airflow in Turbine-Powered Propulsion Simulators.
Publication Date Nov 1985
Media Count 17p
Personal Author S. C. Smith
Abstract The development of turbine-powered propulsion simulators for high-speed wind tunnel models requires a bellmouth inlet which can accurately measure compressor-inlet airflow. A bellmouth inlet was instrumented with total pressure probes, static pressure pro ...
Keywords Air flow
Compressible flow
Flow geometry
Flow measurement
Inlet flow
Mach number
Reynolds number
Wind tunnels
Source Agency National Aeronautics and Space Administration
NTIS Subject Category 51F - Test Facilities & Equipment
Corporate Author National Aeronautics and Space Administration, Moffett Field, CA. Ames Research Center.
Document Type Technical report
Title Note N/A
NTIS Issue Number 8604
Contract Number N/A

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