Vortex sensing tests at NAFEC.

Burnham, D. C.; Hallock, J. N.; Kodis, R,; Sullivan, T.

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Vortex sensing tests at NAFEC.

1972-01-01
By Burnham, D. C. ; Hallock, J. N. ; Kodis, R, ; ...

File Language:

English

Details

Creators:

Burnham, D. C. ; Hallock, J. N. ; Kodis, R, ; Sullivan, T.
Corporate Creators:

John A. Volpe National Transportation Systems Center (U.S.)
Subject/TRT Terms:

Acoustic Detectors Detectors Flow Hot Wire Anemometry Pressure Remote Sensing Vortices Wakes Wing Tip Vortices
Publication/ Report Number:

DOT-TSC-FAA-72-2
Resource Type:

Tech Report
Corporate Publisher:

United States. Department of Transportation. Federal Aviation Administration
Abstract:

The report describes the results of a series of tests to determine and evaluate three experimental techniques for remote sensing of the wing-tip vortices generated by heavy commercial and military aircraft. These techniques involved a pulsed, bistatic acoustic detection and ranging system (referred to as an acoustic radar); a ground level pressure sensor, and a ground level hot-wire anemometer. Results in the form of altitudes and times of tower hits and vortex tracks are presented and compared to the tower data wherever possible.
Format:

PDF
Collection(s):

Volpe Center
Main Document Checksum:

urn:sha256:35378981962373197b6e31d5241a806ab8071eeb3029c27e504f73579e949ae3
Download URL:

https://rosap.ntl.bts.gov/view/dot/9172/dot_9172_DS1.pdf
File Type:

[PDF - 2.97 MB ]

File Language:

English

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