Aircraft wake vortex core size measurements

21st AIAA Applied Aerodynamics Conference

Volumn , Issue , 2003, Pages

  Delisi, Donald P ^a   Greene, George C ^b   Robins, Robert E ^a   Vicroy, Dan C ^b   Wang, Frank Y ^c  

^a NORTHWEST RESEARCH ASSOCIATES   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c VOLPE NATIONAL TRANSPORTATION SYSTEMS CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT; COMPUTATIONAL FLUID DYNAMICS; NUMERICAL MODELS; SMOKE; TESTING; VELOCITY; WAKES;

AIRCRAFT WAKE VORTICES; CONTINUOUS WAVE; JOHN F. KENNEDY INTERNATIONAL AIRPORT; LOCKHEED MARTIN; RADIAL DISTANCE; TANGENTIAL VELOCITIES; TRAILING VORTEX; VELOCITY VORTICES;

VORTEX FLOW;

EID: 85067320539     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-3811     Document Type: Conference Paper

References (19)

1. Proctor, F.H., 1996: Numerical Simulation of Wake Vortices Measured During the Idaho Falls and Memphis Field Programs, AIAA Paper 96-2496, 14th AIAA Applied Aerodynamic Conference, New Orleans.
2. Robins, R.E. and D.P. Delisi, 1997: Numerical Simulations of Three-Dimensional Trailing Vortex Evolution, AIAA Journal, 35, pp. 1552-1555.
3. Proctor, F.H. and J. Han, 1999: Numerical study of Wake Vortex Interaction with the Ground Using the Terminal Area 4 Simulation System, AIAA Paper No. 99-0754, 37th Aerospace Sciences Meeting & Exhibit, Reno.
4. Han, J., Y-L. Lin, S.P. Arya, and F.H. Proctor, 2000: Numerical Study of Wake Vortex Decay and Descent in Homogeneous Atmospheric Turbulence, AIAA Journal, 38, pp. 643-656.
5. Delisi, D.P. and R.E. Robins, 2000: Short-Scale Instabilities in Trailing Wake Vortices in a Stratified Fluid, AIAA Journal, 38, pp. 1916-1923.
6. Vicroy, D.D., P.M. Vijgen, H.M. Reimer, J.L. Gallegos, and P.R. Spalart, 1998: Recent NASA Wake-Vortex Flight Tests, Flow-Physics Database and Wake-Development Analysis, Paper 985592, 1998 World Aviation Conference, Anaheim.
7. Burnham, D.C, and J.N. Hallock, 1982: Chicago Monostatic Acoustic Vortex Sensing System, Volume IV: Wake Vortex Decay, FAA-RD-79-103, IV, Transportation Systems Center, Cambridge, MA, July.
8. Tombach, I., 1973: Observations of Atmospheric Effects on Vortex Wake Behavior, Journal of Aircraft, 10, pp.641-647.
9. Lissaman, P.B.S., S.C. Crow, P.B. MaCcready Jr., I.H. Tombach, and E.R. Bate Jr., 1973: Aircraft Vortex Wake Descent and Decay under Real Atmospheric Effects, FAA-RD-73-120, AeroVironment Inc., Pasadena, CA, October.
10. Garodz, L.J. and K.L. Clawson, 1993: Vortex Wake Characteristics of B757-200 and B767-200 Aircraft Using the Tower Fly-By Technique, NOAA Technical Memorandum ERL ARL-199, January.
11. Robins, R.E., D.P. Delisi, and G.C. Greene, 2001: Algorithm for Prediction of Trailing Vortex Evolution, J. Aircraft, 38, pp. 911-917.
12. Heinrichs, R.M. and T. J. Dasey, 1997: Analysis of Circulation Data from a Wake Vortex Llidar, AIAA Paper No. 97-0059, 35th Aerospace Sciences Meeting & Exhibition, Reno, NV.
13. Nguyen, D.P.C., 1998: Wake Vortex JFK2, RTI/4903-032-03S, Research Triangle Institute, prepared for NASA Langley Research Center, Hampton, VA, August.
14. Robins, R.E. and D.P. Delisi, 1998: Numerical Simulations of Three-Dimensional Trailing Vortex Evolution in Stratified Fluid, AIAA Journal, 36, 981-985.
15. Zheng, Z.C. and K. Baek, 1999: N-S Simulations of Crow-type Instabilities in Vortex Wake, AIAA Paper No. 99-0981, 37th Aerospace Sciences Meeting and Exhibition, Reno, NV.
16. Proctor, F.H., D.W. Hamilton, and J. Han, 2000: Wake Vortex Transport and Decay in Ground Effect: Vortex Linking with the Ground, AIAA Paper No. 2000-0757, 38th Aerospace Sciences Meeting and Exhibition, Reno, NV.
17. Garten, J.F., J. Werne, D.C. Fritts, and S. Arendt, 2001: Direct Simulations of the Crow Instability and Subsequent Vortex Reconnection in a Stratified Fluid, Journal of Fluid Mechanics, 426, pp. 1-45.
18. Rottman, J.W., D.G. Dommermuth, G.E. Innis, T.T. O'Shea, and E. Novikov, 2002: Numerical Simulation of Wakes in a Weakly Stratified Fluid, 24th Symposium on Naval Hydrodynamics, Fukuoka, Japan.
19. Robins, R.E. and D.P. Delisi,. 2003: LES Simulation of High Reynolds Number Trailing Vortex Wakes, DoD HPCMP Users Group Meeting, Bellevue, WA.