Adjoint design methods for nozzles for reduced noise in high-speed jets

Philip John Morris, N. Sikarwar, D. K. McLaughlin, C. W. Kuo, M. Lurie

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (Scopus)

Abstract

This paper describes the use adjoint methods for nozzle design and control optimization to reduce noise in supersonic jets operating at off-design conditions. The motivation for the work is the development of an optimization procedure for a new jet noise reduction concept that involves flow injection into the diverging section of a convergent-divergent nozzle. The noise reduction method and some preliminary flow and acoustic measurements are described. Noise reductions of more than 5dB in mixing noise as well as reductions in broadband shock associated noise are demonstrated. Two adjoint optimization methods are then described. The first example, provided to fix the ideas of adjoint design, involves changing the nozzle contours to achieve a desired pressure distribution in the nozzle. The second example involves the determination of the optimum distribution of blowing and/or suction in the diverging section of the nozzle to achieve a minimization of the shock strength. Following a description of the noise reduction concept and some preliminary results, a general review of adjoint methods in design is given. In adjoint design, a cost function is minimized within defined constraints. These include the requirement that the flow satisfies the flow conservation equations and boundary conditions as well as other smoothness constraints. The sensitivity of the cost function to the design parameters can be obtained from a solution of an adjoint problem. The adjoint problem formulation for two example approaches is given. Results are given in two cases for convergent-divergent nozzles with jets operating at different pressure ratios including an over-expanded condition, which is typical of high performance military aircraft engines on take-off.

Original languageEnglish (US)
Title of host publication48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012
StatePublished - Dec 1 2012
Event48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012 - Atlanta, GA, United States
Duration: Jul 30 2012Aug 1 2012

Other

Other48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012
CountryUnited States
CityAtlanta, GA
Period7/30/128/1/12

Fingerprint

Noise abatement
Nozzles
Cost functions
Nozzle design
Military aircraft
Aircraft engines
Takeoff
Blow molding
Pressure distribution
Conservation
Acoustics
Boundary conditions

All Science Journal Classification (ASJC) codes

  • Energy Engineering and Power Technology
  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering
  • Mechanical Engineering

Cite this

Morris, P. J., Sikarwar, N., McLaughlin, D. K., Kuo, C. W., & Lurie, M. (2012). Adjoint design methods for nozzles for reduced noise in high-speed jets. In 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012
Morris, Philip John ; Sikarwar, N. ; McLaughlin, D. K. ; Kuo, C. W. ; Lurie, M. / Adjoint design methods for nozzles for reduced noise in high-speed jets. 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012. 2012.
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Morris, PJ, Sikarwar, N, McLaughlin, DK, Kuo, CW & Lurie, M 2012, Adjoint design methods for nozzles for reduced noise in high-speed jets. in 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012. 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012, Atlanta, GA, United States, 7/30/12.

Adjoint design methods for nozzles for reduced noise in high-speed jets. / Morris, Philip John; Sikarwar, N.; McLaughlin, D. K.; Kuo, C. W.; Lurie, M.

48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012. 2012.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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Morris PJ, Sikarwar N, McLaughlin DK, Kuo CW, Lurie M. Adjoint design methods for nozzles for reduced noise in high-speed jets. In 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012. 2012