02309cam a2200349Ma 4500011445062MiAaHDL20141009010000.0m d cr bn ---auaua030904s1972 dcua f000 0 eng dsdr-uiuc6403879(OCoLC)643056129EGMSTFUIUUNAS 1.14:D-6655NASA-TN-D-6655Andrews, William H.Exploratory flight investigation of aircraft response to the wing vortex wake generated by jet transport aircraft /William H. Andrews, Glenn H. Robinson, and Richard R. Larson.NASA TN D-6655Washington, D.C. :National Aeronautics and Space Administration :[For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151],1972.31 p. :ill. ;27 cm.NASA technical note ;D-6655The effect of intercepting wing tip vortices generated by large jet transports, including jumbo jets, over separation distances from 1 nautical mile to 15 nautical miles is evaluated on the basis of the response of a vortex probe airplane in the roil mode. The vortex probe test aircraft included a representative general aviation airplane, an executive jet, a fighter, and light and medium weight jet transports. The test conditions and airplane configurations were comparable to those normally used during takeoff, landing, or holding pattern operations. For flight safety the tests were performed at altitudes from 9500 feet to 12,500 feet. In addition to an evaluation of the probe airplane response, a flight test technique is suggested for determining minimum separation distance, using as variable the ratio of vortex-induced roll acceleration to maximum lateral control acceleration and the gross weight of the generating aircraft.Mode of access: Internet.Airplanes, MilitaryFlight testing.Jet transports.Wakes (Aerodynamics)Aerodynamics.Vortex-motion.Larson, Richard R.Robinson, Glenn H.Flight Research Center (U.S.)United States.National Aeronautics and Space Administration.01144506220101110144710.020141009010000.020141112165512.02025-01-02T19:12:33Z2025-01-02T18:30:02ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc6403879uiugSDRUIUCuiug.30112106882951UIU6403879UIUUIUC20250102googleuiug.301121068829511972pdbibUS fed doc