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Flight test investigation of the vortex wake characteristics behind a Boeing 727 during two-segment and normal ILS approaches (A joint NASA/FAA report)Flight tests were performed to evaluate the vortex wake characteristics of a Boeing 727 aircraft during conventional and two-segment instrument landing approaches. Smoke generators were used for vortex marking. The vortex was intentionally intercepted by a Lear Jet and a Piper Comanche aircraft. The vortex location during landing approach was measured using a system of phototheodolites. The tests showed that at a given separation distance there are no readily apparent differences in the upsets resulting from deliberate vortex encounters during the two types of approaches. The effect of the aircraft configuration on the extent and severity of the vortices is discussed.
Document ID
19750009268
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Barber, M. R.
(NASA Flight Research Center Edwards, CA, United States)
Kurkowski, R. L.
(NASA Flight Research Center Edwards, CA, United States)
Garodz, L. J.
(NASA Flight Research Center Edwards, CA, United States)
Robinson, G. H.
(NASA Flight Research Center Edwards, CA, United States)
Smith, H. J.
(NASA Flight Research Center Edwards, CA, United States)
Jacobsen, R. A.
(NASA Flight Research Center Edwards, CA, United States)
Stinnett, G. W., Jr.
(NASA Flight Research Center Edwards, CA, United States)
Mcmurtry, T. C.
(NASA Flight Research Center Edwards, CA, United States)
Tymczyszyn, J. J.
(NASA Flight Research Center Edwards, CA, United States)
Devereaux, R. L.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1975
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
FAA-NA-75-151
NASA-TM-X-62398
Report Number: FAA-NA-75-151
Report Number: NASA-TM-X-62398
Accession Number
75N17340
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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