Active inlet flow control technology demonstration

Aeronautical Journal

Volumn 104, Issue 1040, 2000, Pages 473-479

  Hamstra, J W ^a   Miller, D N ^a   Truax, P P ^a   Anderson, B A ^a   Wendt, B J ^a  

^a NONE

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; ASPECT RATIO; COMPUTATIONAL FLUID DYNAMICS; DUCTS; FLOW CONTROL; JETS; MATHEMATICAL MODELS; PRESSURE DROP; REYNOLDS NUMBER; TURBULENCE; VORTEX FLOW;

ACTIVE INLET FLOW CONTROL; MICROVANE VORTEX GENERATORS; SECONDARY FLOW CONTROL; SEPARATION CONTROL;

SUBSONIC AERODYNAMICS;

EID: 0034291412     PISSN: 00019240     EISSN: None     Source Type: Trade Journal    
DOI: None     Document Type: Article

References (13)

1. TINDELL, R.H. Highly compact inlet diffuser technology, AIAA Paper 87-1747.
2. AMITAY, M., PITT, D., KIBENS, V., PAREKH, D. and GLEZER, A. Control of internal flow separation using synthetic jet actuators, AIAA Paper 2000-0903.
3. ANDERSON, B.H. and GIBB, J. Study on vortex generator flow control for the management of inlet distortion, J Propulsion and Power, 1993, 9, (3), pp 420-430.
4. ANDERSON, B.H. and GIBB, J. Vortex generator installation studies on steady state and dynamic distortion, J Aircr, 1998, 35, (4), pp 513-552.
5. GIBB, J. and ANDERSON, B.H. Vortex flow control applied to aircraft intake ducts, Proceedings of the Royal Aero Society, Conf Paper, 1995, 14.
6. BRAY, T.P., WIER, B. and GIBB, J. Experimental evaluation of inlet distortion management at flight Reynolds number, DERA/MSS/MSFC2/CR990134, 1999.
7. BENDER, E.E., ANDERSON, B.H. and YAGLE, P.J. Vortex generator modelling for Navier-Stokes codes, ASME Paper No FEDSM99-69219.
8. ANDERSON, B.H., MILLER, D.N., YAGLE, P.J. and TRUAX, P.P. A study on MEMS flow control for the management of engine face distortion in compact inlet systems. ASME Paper No FEDSM99-6920.
9. BOX, E.P., HUNTER, W.G. and HUNTER, J.S. Statistics for Experimenters, John Wiley & Sons, 1978.
10. MILLER, D.N., YAGLE, P.J. and HAMSTRA, J.W. Fluidic throat skewing for thrust vectoring in fixed-geometry nozzles, AIAA Paper 99-0365.
11. HERCOCK, R.G. and WILLIAMS, D.D. Aerodynamic response, AGARD-LS-72, Paper 3, 1974.
12. WENDT, B.J. and REICHERT, B.A. An inexpensive and effective five-hole probe rake, Experiments in fluids, 1995, 19, pp. 295-296.
13. REICHERT, B.A. and WENDT, B.J. Uncertainty of five-hole probe measurements. Fluid Measurement and Instrumentation, 1994, 183, pp 39-44.