Reduction of jet penetration in a cross-flow by using tabs

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 1998, Pages

  Zaman, K B M Q ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

NOZZLES; PROPULSION; WIND TUNNELS;

FILM COOLING; FLOW BLOCKAGE; JET PENETRATION; LATERAL SPREADING; MOMENTUM RATIO; NOZZLE DIAMETER; PRESSURE LOSS; WIND TUNNEL EXPERIMENT;

DELTA WING AIRCRAFT;

EID: 85088198414     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-3276     Document Type: Conference Paper

References (5)

1. Liscinsky, D.S., True, B. and Holdeman, J.D., "Effects of initial conditions on a single jet in crossflow", AIM Paper 95-2998, 31st Joint Prop Conf, San Diego, July 10-12,1995.
2. Zaman, K.B.M.Q. and Foss, J.K., "The effect of vortex generators on a jet in a cross-flow", Physics of Fluids, vol. 9 (1), pp. 106-114,1997.
3. Zaman K.B.M.Q., Reeder M.F., & Samimy M., "Control of an axisymmetric jet using vortex generators", Physics of Fluids A, 6 (2), pp. 778-793, 1994.
4. Hippensteele, S., "Film-cooling heat transfer measurements using liquid crystals", Proc. Coolant Flow Management Workshop, Dec. 12- 13,1996, NASA CP10195.
5. Abramovich, G.N., "The theory of turbulent jets", TheM/T. Press, 1963.