Distributed hingeless flow control and rotary synthetic jet actuation

Lance Traub, Adam Miller, Puneet Singla, Monish Tandale, John Junkins, Othon Rediniotis, Matthew Zeiger

Research output: Contribution to conferencePaper

2 Citations (Scopus)

Abstract

In this paper, a continuing research effort is detailed aimed at effecting practical hinge-less closed-loop flow control of wings. The systematic evolution of synthetic/pneumatic actuators suitable for this purpose, via distributed actuation, is described as is their effectiveness as flow control tools. The synthetic jet mechanisms are based on automotive technology; piston to Wankel-rotary, with the piston or rotor acting as the compressor. Control methodologies, for both controlling the DC motors, driving the synthetic jet actuators (SJA) as well as controlling the wing in free-to-pitch motions were developed. Methods of implementing and distributing the actuation, so as to allow pitch control at both low and high angles of attack are presented. High angle of attack control facilitated through upper surface separation control (with the SJA located close to the leading edge and ejecting its jet tangential to the surface) was shown to be effective and controllable. However, at low incidence, this geometric implementation is ineffective. For these conditions, a wind tunnel investigation was undertaken to examine the possibility of using a jet flap for hinge-less control. Tests encompassed jet momentum coefficient variation and comparison with a Gurney flap located at the same location. The data showed that the jet flap generates lift and moment coefficient increments similar to a 0.75% of chord Gurney flap for moderate jet momentum coefficients.

Original languageEnglish (US)
Pages2284-2313
Number of pages30
StatePublished - Jul 1 2004
Event42nd AIAA Aerospace Sciences Meeting and Exhibit - Reno, NV, United States
Duration: Jan 5 2004Jan 8 2004

Other

Other42nd AIAA Aerospace Sciences Meeting and Exhibit
CountryUnited States
CityReno, NV
Period1/5/041/8/04

Fingerprint

Flow control
Jet flaps
Hinges
Angle of attack
Pistons
Momentum
Actuators
Pneumatic actuators
DC motors
Wind tunnels
Compressors
Rotors

All Science Journal Classification (ASJC) codes

  • Engineering(all)

Cite this

Traub, L., Miller, A., Singla, P., Tandale, M., Junkins, J., Rediniotis, O., & Zeiger, M. (2004). Distributed hingeless flow control and rotary synthetic jet actuation. 2284-2313. Paper presented at 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, United States.
Traub, Lance ; Miller, Adam ; Singla, Puneet ; Tandale, Monish ; Junkins, John ; Rediniotis, Othon ; Zeiger, Matthew. / Distributed hingeless flow control and rotary synthetic jet actuation. Paper presented at 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, United States.30 p.
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Traub, L, Miller, A, Singla, P, Tandale, M, Junkins, J, Rediniotis, O & Zeiger, M 2004, 'Distributed hingeless flow control and rotary synthetic jet actuation' Paper presented at 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, United States, 1/5/04 - 1/8/04, pp. 2284-2313.

Distributed hingeless flow control and rotary synthetic jet actuation. / Traub, Lance; Miller, Adam; Singla, Puneet; Tandale, Monish; Junkins, John; Rediniotis, Othon; Zeiger, Matthew.

2004. 2284-2313 Paper presented at 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, United States.

Research output: Contribution to conferencePaper

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Traub L, Miller A, Singla P, Tandale M, Junkins J, Rediniotis O et al. Distributed hingeless flow control and rotary synthetic jet actuation. 2004. Paper presented at 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, United States.