NASA aircraft vortex spacing system development status

37th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1999, Pages

  Hinton, David A ^a   Charnock, James K ^a   Bagwell, Donald R ^a   Grigsby, Donner ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; AIRCRAFT MANUFACTURE; AIRPORTS; FLIGHT DYNAMICS; METEOROLOGY; NASA; REAL TIME SYSTEMS; WAKES;

ENGINEERING MODELING; INSTRUMENT METEOROLOGICAL CONDITIONS; INTERNATIONAL AIRPORT; NASA LANGLEY RESEARCH CENTER; OPERATIONAL EXPERIENCE; OPERATIONAL SYSTEMS; REAL-TIME OPERATION; SYSTEM ARCHITECTURES;

VORTEX FLOW;

EID: 84983122289     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-753     Document Type: Conference Paper

References (24)

1. Hinton, David A.: Aircraft Vortex Spacing System (AVOSS) Conceptual Design, NASA TM110184, August 1995.
2. Hinton, D.A.: An Aircraft Vortex Spacing System (AVO~S) For Dynamical Wake Vortex Spacing Criteria, AGARD 78th Fluid Dynamics Panel Meeting and Symposium on the Characterisation & Modification of Wakes from Lifting Vehicles in Fluids, Trondheim, Norway, 2023 May, 1996, AGARD CP-584, Paper 23.
3. Perry, R. Brad; Hinton, David A.; and Stuever, Robert A.: NASA Wake Vortex Research for Aircraft Spacing, AIAA 97-0057, 35th Aerospace Sciences Meeting & Exhibit, January 9-10,1997, Reno, NV.
4. Matthews, Michael P. and Denneno, Andrew P.; Integration of Multiple Meteorological Sensor Observations for Wake Vortex Behavior Comparison, 79th AMS Annual Meeting, Eighth Conference on Aviation, Range, and Aerospace Meteorology 10-15 January 1999, Dallas, TX, Paper #11.1
5. Robins, Robert E.; Delisi, Donald P.; Greene, George C.: Development and Validation of a Wake Vortex Prediction Algorithm, AIAA 98-0665, 36th Aerospace Sciences Meeting & Exhibit, January 12-15,1998, Reno, NV.
6. Campbell, S.D.; Dasey, T.J.; Freehart, R.E.; Heinrichs, R.M.; Matthews, M.P.; Perras, G.H.; Rowe, G.S.: Wake Vortex Field Measurement Program at Memphis, TN Data Guide, Lincoln Laboratory Project Report NASA/L-2, January 14, 1997. Also published as NASA CR-201690, April 1997.
7. Heinrichs, Richard M.; Dasey, Timothy J.; Matthews, Michael P.; Campbell, Steven D.; Freehart, Robert E.; Perras, Glenn H.; and Salamitou, Philippe: Measurements of Aircraft Wake Vortices at Memphis International Airport with a CW C02 Coherent Laser Radar, SPIE2737-20, SPIE Symposium on Aerospace/Defense Sensing and Controls, Air Traffic Control Technologies II session, April 8-11, 1996, Orlando, FL.
8. th conference on Coherent Laser Radar, Linkoping, Sweden, June 1997.
9. Burnham, D.; Gorstein, M.; Hallock, IN; Kodis, R; Sullivan, T; McWilliams, I.G.: Aircraft Wake Vortex Sensing Systems, DOT-TSC-FAA-72-13, June 1971.
10. Greene, George C.: An Approximate Model of Vortex Decay in the Atmosphere, AIAA 85-1835CP, August 1985, See also Journal of Aircraft, Vol. 23, No.7, July 1986, pp. 566-573.
11. Liu, H.T.; Hwang, P.A.; and Srnsky, R.A.: Physical Modeling of Ground Effects on Vortex Wakes, Journal of Aircraft, Vol. 29, No.6, Nov Dec 1992.
12. Proctor, F.H.; Hinton, D.A.; Han, J.; Schowalter, D.G.; and Lin, Y.-L.: Two Dimensional Wake Vortex Simulations in the Atmosphere: Preliminary Sensitivity Studies, AIAA 97-0056, Presented at the 35th Aerospace Sciences Meeting & Exhibit, January 9-10,1997, Reno, NV.
13. Zak, J. Allen and Rodgers, William G.: Documentation of Atmospheric Conditions During Observed Rising Aircraft Wakes, NASA CR-4767, April 1997.
14. Hinton, David A. and Tatnall, Chris R.: A Candidate Wake Vortex Strength Definition for Application to the NASA Aircraft Vortex Spacing System (AVOSS), NASA TM-110343, September 1997.
15. Proctor, Fred H.: The NASA-Langley Wake Vortex Modeling Effort in Support of an Operational Aircraft Spacing System, AIAA 980589, 36th Aerospace Sciences Meeting & Exhibit, January 12-15,1998, Reno, NV.
16. Sarpkaya, T.: Decay of Wake Vortices of Large Aircraft, AIAA 98-0592, 36th Aerospace Sciences Meeting & Exhibit, January 12-15, 1998, Reno, NV. Also see AIAA Journal, Vol. 36, Number 9, Pages 1671-1679.
17. th Conference on Numerical Weather Prediction, Amer. Meteor. Soc., January 11-16, 1998, pp 6568.
18. Heinrichs, R. M., Dasey, T. J., Matthews, M. P., Campbell, S. D., Freehart, R. E., and G. P. Perras: Measurements of Aircraft Wake Vortices at Memphis International Airport with a CW C02 Coherent Laser Radar, Proc. Intl. Soc. for Optical Eng. (SPIE), Vol. 2737: 122-133, 1996.
19. Marshall, Robert E.; Mudukutore, Ashok; and Wissel, Vicki L. H.: Radar Reflectivity in Wingtip Generated Wake Vortices, NASA/CR-97-206259, December 1997.
20. Safety Issues Related to Wake Vortex Encounters During Visual Approach to Landing, NTSB Special Investigation Report NTSB/SIR94/01 Notation 6264, February, 1994.
21. Stewart, Eric C.: A Piloted Simulation Study of Wake Turbulence on Final Approach, AIAA Atmospheric Flight Mechanics Conference and Exhibit, AIAA-98-4339, August 10-12, 1998.
22. Garodz, Leo J. and Clawson, Kirk: Vortex Wake Characteristics of B757-200 and B767-200 Aircraft Using the Tower Fly-By Technique, NOAA Technical Memorandum ERL-ARL-199, January, 1993.
23. th AIAA Applied Aerodynamics Conference Proceedings Part-2, June 17-20, 1996, pgs. 943-960; New Orleans, LA.
24. Tatnall, Christopher Rhoads: A Proposed Methodology for Determining Wake-Vortex Imposed Aircraft Separation Constraints, A Thesis submitted to the School of Engineering and Applied Science, The George Washington University, August, 1995.