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Unsteady loads due to propulsive lift configurations. Part B: Pressure and velocity measurements in a three dimensional wall jetThe effects of increasing the velocity ratio, lambda sub j were explored. The quantities measured include the width of the mixing region, the mean velocity field, turbulent intensities and time scales. In addition, wall and static pressure velocity correlations and coherences are presented. The velocity measurements were made using a laser Doppler velocimeter with a phase locked loop processor. The fluctuating pressures were monitored using condenser type microphones.
Document ID
19780012125
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Catalano, G. D.
(Virginia Univ. Charlottesville, VA, United States)
Morton, J. B.
(Virginia Univ. Charlottesville, VA, United States)
Humphris, R. R.
(Virginia Univ. Charlottesville, VA, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1978
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-156121
UVA/528095/MAE78/115-PT-B
UVA/526033/MAE78/101-PT-B
Report Number: NASA-CR-156121
Report Number: UVA/528095/MAE78/115-PT-B
Report Number: UVA/526033/MAE78/101-PT-B
Accession Number
78N20068
Funding Number(s)
CONTRACT_GRANT: NGR-47-005-219-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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