Skip to main content

2019 | OriginalPaper | Buchkapitel

3. Operational Modal Analysis of a Thin-Walled Rocket Nozzle Using Phase-Based Image Processing and Complexity Pursuit

verfasst von : Marc A. Eitner, Benjamin G. Miller, Jayant Sirohi, Charles E. Tinney

Erschienen in: Rotating Machinery, Optical Methods & Scanning LDV Methods, Volume 6

Verlag: Springer International Publishing

Aktivieren Sie unsere intelligente Suche, um passende Fachinhalte oder Patente zu finden.

search-config
loading …

Abstract

In this work, the modal parameters of a reduced scale, thin-walled, metallic rocket nozzle are extracted through Operational Modal Analysis (OMA). The specimen is excited using pressurized gas from a rocket nozzle test stand. Deformation of the nozzle lip is measured using a non-contact optical technique consisting of two-dimensional marker tracking in conjunction with phase-based motion amplification. OMA methods that use digital image data suffer from low signal to noise ratios (SNR), especially in higher modes with small amplitude vibrations. The structural displacements are often on a subpixel scale and therefore difficult to analyze without additional image processing. Phase-based motion amplification (PMA) offers a possible solution to this problem by magnifying subpixel motion. This work focuses on the implementation of the technique in a marker-tracking algorithm, which serves to extract the time-history of high-contrast markers placed on a large area ratio nozzle with a 5.3 inch exit diameter. Grayscale images taken with a high-speed camera are first processed with the phase-based algorithm to increase the marker motion in a certain broad frequency band. This results in a set of modified images, which are then analyzed with a tracking algorithm that identifies centroid positions of fluorescent markers. The time-history of these markers is then used as input for an OMA algorithm, namely the Complexity Pursuit algorithm, which leads to estimates of eigenfrequencies, damping ratios and mode shapes. A quantitative comparison between the modal parameters obtained with and without additional motion magnification is provided. Results of a numerical simulation are provided that demonstrate the improvement of estimated modal parameters. The modal parameters of the first six modes of the nozzle are found using this method. The motion was amplified in the range of 0–1400 Hz which includes the six eigenfrequencies. Without application of the broad band PMA, the highest mode cannot clearly be identified and the quality of the other modes decreases.

Sie haben noch keine Lizenz? Dann Informieren Sie sich jetzt über unsere Produkte:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

  • über 102.000 Bücher
  • über 537 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Maschinenbau + Werkstoffe
  • Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 390 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Maschinenbau + Werkstoffe




 

Jetzt Wissensvorsprung sichern!

Fußnoten
1
i-SPEED 726 monochromatic camera manufactured by ix Cameras™.
 
Literatur
1.
Zurück zum Zitat Baars, W.J., Tinney, C.E., Ruf, J.H., Brown, A.M., McDaniels, D.M.: Wall pressure unsteadiness and side loads in overexpanded rocket nozzles. AIAA J. 50(1), 61–73 (2012)CrossRef Baars, W.J., Tinney, C.E., Ruf, J.H., Brown, A.M., McDaniels, D.M.: Wall pressure unsteadiness and side loads in overexpanded rocket nozzles. AIAA J. 50(1), 61–73 (2012)CrossRef
2.
Zurück zum Zitat Baars, W.J., Tinney, C.E., Ruf, J.H.: Non-stationary shock motion unsteadiness in an axisymmetric geometry with pressure gradient. Exp. Fluids. 56(92), 1–18 (2015) Baars, W.J., Tinney, C.E., Ruf, J.H.: Non-stationary shock motion unsteadiness in an axisymmetric geometry with pressure gradient. Exp. Fluids. 56(92), 1–18 (2015)
3.
Zurück zum Zitat Blades, E.L., Luke, E.A., Ruf, J.: Fully coupled fluid-structure interaction simulation of rocket engine side loads. 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA Paper 2012–3969, Atlanta, Georgia, 30July–1 Aug 2012 Blades, E.L., Luke, E.A., Ruf, J.: Fully coupled fluid-structure interaction simulation of rocket engine side loads. 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA Paper 2012–3969, Atlanta, Georgia, 30July–1 Aug 2012
4.
Zurück zum Zitat Tinney, C.E., Scott, K., Routen, M., Sirohi, J., Ruf, J.: Effect of aeroelasticity on vibroacoustic loads during startup of large area ratio nozzles. 23rd AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2017-3361, Denver, Colorado, 5–9 June 2017 Tinney, C.E., Scott, K., Routen, M., Sirohi, J., Ruf, J.: Effect of aeroelasticity on vibroacoustic loads during startup of large area ratio nozzles. 23rd AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2017-3361, Denver, Colorado, 5–9 June 2017
5.
Zurück zum Zitat Stone, J.V.: Blind source separation using temporal predictability. Neural Comput. 13(7), 1559–1574 (2001)CrossRef Stone, J.V.: Blind source separation using temporal predictability. Neural Comput. 13(7), 1559–1574 (2001)CrossRef
6.
Zurück zum Zitat Wadhwa, N., Rubenstein, M., Fredo, D., Freeman, W.T.: Phase-based video motion processing. ACM Trans. Graph. 32(4), 80:1–80:10 (2013)CrossRef Wadhwa, N., Rubenstein, M., Fredo, D., Freeman, W.T.: Phase-based video motion processing. ACM Trans. Graph. 32(4), 80:1–80:10 (2013)CrossRef
7.
Zurück zum Zitat Poozesh, P., Sarrafi, A., Mao, Z., Avitabile, P., Niezrecki, C.: Feasibility of extracting operating shapes using phase-based motion magnification technique and stereo-photogrammetry. J. Sound Vib. 407, 350–366 (2017)CrossRef Poozesh, P., Sarrafi, A., Mao, Z., Avitabile, P., Niezrecki, C.: Feasibility of extracting operating shapes using phase-based motion magnification technique and stereo-photogrammetry. J. Sound Vib. 407, 350–366 (2017)CrossRef
8.
Zurück zum Zitat Yang, Y., Dorn, C., Mancini, T., Talken, Z., Kenyon, G., Farrar, C., Mascarenas, D.: Blind identification of full-field vibration modes from video measurements with phase-based video motion magnification. Mech. Syst. Signal Process. 85, 567–590 (2017)CrossRef Yang, Y., Dorn, C., Mancini, T., Talken, Z., Kenyon, G., Farrar, C., Mascarenas, D.: Blind identification of full-field vibration modes from video measurements with phase-based video motion magnification. Mech. Syst. Signal Process. 85, 567–590 (2017)CrossRef
9.
Zurück zum Zitat Simoncelli, E.P., Freeman, W.T.: The steerable pyramid: a flexible architecture for multi-scale derivative computation. In: Proceedings of the 1995 International Conference on Image Processing, Washington, DC, 23–26 Oct 1995 Simoncelli, E.P., Freeman, W.T.: The steerable pyramid: a flexible architecture for multi-scale derivative computation. In: Proceedings of the 1995 International Conference on Image Processing, Washington, DC, 23–26 Oct 1995
10.
Zurück zum Zitat Simoncelli, E.P., Freeman, W.T., Adelson, E.H., Heeger, D.J.: Shiftable multi-scale transforms. IEEE Trans. Inf. Theory. 38(2), 587–607 (1992)CrossRef Simoncelli, E.P., Freeman, W.T., Adelson, E.H., Heeger, D.J.: Shiftable multi-scale transforms. IEEE Trans. Inf. Theory. 38(2), 587–607 (1992)CrossRef
11.
Zurück zum Zitat Meirovitch, L.: Fundamentals of Vibration. McGraw-Hill, New York (2001)CrossRef Meirovitch, L.: Fundamentals of Vibration. McGraw-Hill, New York (2001)CrossRef
12.
Zurück zum Zitat Valdez, J.A., Tinney, C.E.: Measurements of a Mach 3 jet using high-speed optical flow techniques. AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2018-3148, Atlanta, Georgia, 25–29 June 2018 Valdez, J.A., Tinney, C.E.: Measurements of a Mach 3 jet using high-speed optical flow techniques. AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2018-3148, Atlanta, Georgia, 25–29 June 2018
Metadaten
Titel
Operational Modal Analysis of a Thin-Walled Rocket Nozzle Using Phase-Based Image Processing and Complexity Pursuit
verfasst von
Marc A. Eitner
Benjamin G. Miller
Jayant Sirohi
Charles E. Tinney
Copyright-Jahr
2019
DOI
https://doi.org/10.1007/978-3-030-12935-4_3

    Marktübersichten

    Die im Laufe eines Jahres in der „adhäsion“ veröffentlichten Marktübersichten helfen Anwendern verschiedenster Branchen, sich einen gezielten Überblick über Lieferantenangebote zu verschaffen.