NTL Record

Title Flight test investigation of rotorcraft wake vortices in forward flight.
Record ID 56241
Personal Name
Creator
Teager, Stephen A.; Biehl, Keith J.; Garodz, Leo J.; Tymczyszym, Joseph J.; Burnham, David C.
Source 94p. in various pagings
Corporate Creator Federal Aviation Administration Technical Center (U.S.); United States. Department of Transportation. Federal Aviation Administration; Scientific and Engineering Solutions, Inc.
Publisher Federal Aviation Administration Technical Center (U.S.)
Publication Date 19960200
Language English
Abstract This report presents the results of helicopter flight test and wake vortex measurements which were designed to provide data necessary for the assessment of hazards to following aircraft. The tests described in this report were conducted using small probe airplanes and a Laser Doppler Velocimeter for wake vortex measurements during forward-flight helicopter operations. Four helicopters, having weight ranging from 7,600 to 70,000 pounds, were used in the test as the wake vortex generating aircraft. Wake vortex strength and decay characteristics as determined from the flight test results are discussed. In the absence of encounter measurements for the case of hover flight, it is recommended that small airplanes, at the same altitude and downwind of a hovering helicopter, maintain at lease 500 feet of separation.
Rosap ID dot:12234
Rosap URL https://rosap.ntl.bts.gov/view/dot/12234
TRT Terms Wakes; Flow; Vortices; Helicopters; Rotary wing aircraft; Laser doppler velocimeters; Tests; Flight tests; Boundary layer separation; Hazards
General Subjects Wake votices
Classification NTL - AVIATION - AVIATION;
NTL - AVIATION - Aviation Safety/Airworthiness
Geographical
Coverage
Alabama; New Jersey
Report Number DOT/FAA/CT-94/117
Availability Volpe National Transportation Systems Center, Technical Reference Center
Resource type Tech Report
URL https://ntlrepository.blob.core.windows.net/lib/56000/56200/56241/DOT-FAA-CT-94-117_WithCorrectedFig4-14.pdf
Format PDF
Database NTL Digital Repository