NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Laser Doppler velocimeter system simulation for sensing aircraft wake vorticesA hydrodynamic model of aircraft vortex wakes in an irregular wind shear field near the ground is developed and used as a basis for modeling the characteristics of a laser Doppler detection and vortex location system. The trailing vortex sheet and the wind shear are represented by discrete free vortices distributed over a two-dimensional grid. The time dependent hydrodynamic equations are solved by direct numerical integration in the Boussinesq approximation. The ground boundary is simulated by images, and fast Fourier Transform techniques are used to evaluate the vorticity stream function. The atmospheric turbulence was simulated by constructing specific realizations at time equal to zero, assuming that Kolmogoroff's law applies, and that the dissipation rate is constant throughout the flow field. The response of a simulated laser Doppler velocimeter is analyzed by simulating the signal return from the flow field as sensed by a simulation of the optical/electronic system.
Document ID
19750010193
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Thomson, J. A. L.
(Physical Dynamics, Inc. Berkeley, CA, United States)
Meng, J. C. S.
(Physical Dynamics, Inc. Berkeley, CA, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1974
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-CR-120624
PD-74-058
Report Number: NASA-CR-120624
Report Number: PD-74-058
Accession Number
75N18265
Funding Number(s)
CONTRACT_GRANT: NAS8-28984
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available