The DOI matches its Crossref record.
Impact identification of stiffened composite panels: I. System development
Open accessAbstract
An investigation was conducted to develop a real-time identification technique for the prediction of the location and force history of low-velocity impacts on composite panels with beam stiffeners. The investigation included both analysis and experiments. Measurements from built-in piezoceramic sensors were used to reconstruct the force history using the smoother-filter algorithm. Impact location was determined by minimizing the difference between modeled response and actual response. Computer codes were developed for model construction (WFMODEL) and impact identification (WIDIMPACT). The model allowed for the variation of plate structural properties (density and stiffness) due to the presence of stiffeners. Results of extensive experiments verified the model, as coded in WFMODEL, for impacts both in the bay and on the stiffener. The identification technique, as implemented in the code WIDIMPACT, demonstrated real-time capability. Good agreement was found between predicted and actual force history and location, with success for different impact masses.
Overview
The claims and statistics of this paper haven’t been checked yet.
Run the check — free, no account needed. It reads the open-access text and checks the sources it cites.
Integrity signals
Registry
Cites
Statistics
Verification
Claims the paper makes
The claims and statistics of this paper haven’t been checked yet.
Run the check — free, no account needed. It reads the open-access text and checks the sources it cites.
Self-check
Percentages, sums and reported differences re-computed from the paper’s own numbers.
The self-check needs the paper’s full text.
Citations
Cites
No references could be resolved yet.
Research works printed but not linked: 22
- Miller A G, 1994, Compos. Struct., 27, 193, 10.1016/0263-8223(94)90080-9 · doi:10.1016/0263-8223(94)90080-9
- 10.1016/S0263-8223(98)00089-0 · DOI
- Siow Y P, 1998, J. Compos. Mater., 32, 1178, 10.1177/002199839803201203 · DOI
- Okafor A C, 1996, Proc. SPIE, 2718, 291, 10.1117/12.240895 · doi:10.1117/12.240895
- Michel L D, 1996, Proc. SPIE, 2779, 230, 10.1117/12.237117 · doi:10.1117/12.237117
- Gunther M F, 1993, Proc. SPIE, 1798, 262, 10.1117/12.141322 · DOI
- Doyle J F, 1987, J. Sound Vib., 118, 441, 10.1016/0022-460X(87)90363-4 · DOI
- 10.1016/0734-743X(95)00022-4 · doi:10.1016/0734-743x(95)00022-4
- Wu E, 1994, AIAA J., 32, 2433, 10.2514/3.12310 · doi:10.2514/3.12310
- Wu E, 1995, Exp. Mech., 35, 11, 10.1007/BF02325828 · doi:10.1007/bf02325828
- Tracy M, 1996, Proc. SPIE, 2779, 118, 10.1117/12.237096 · doi:10.1117/12.237096
- Chandrashekara K, 1996, Proc. SPIE, 2718, 320, 10.1117/12.240871 · doi:10.1117/12.240871
- Akhavan F, 1996, Proc. SPIE, 2839, 277, 10.1117/12.255363 · doi:10.1117/12.255363
- Jones R T, 1997, J. Intell. Mater. Syst. Struct., 7, 90, 10.1177/1045389X9700800109 · doi:10.1177/1045389x9700800109
- Schindler P M, 1995, Proc. SPIE, 2444, 481, 10.1117/12.207698 · doi:10.1117/12.207698
- Joshi S P, 1996, Proc. SPIE, 2718, 185, 10.1117/12.240860 · doi:10.1117/12.240860
- Giles G L, 1986, J. Aircraft, 23, 859, 10.2514/3.45393 · doi:10.2514/3.45393
- Lee H P, 1994, Compos. Struct., 29, 405, 10.1016/0263-8223(94)90109-0 · doi:10.1016/0263-8223(94)90109-0
- Lee H P, 1995, Mech. Struct. Mach., 23, 309, 10.1080/08905459508905239 · doi:10.1080/08905459508905239
- Dugundji J, 1988, AIAA J., 26, 1013, 10.2514/3.10005 · doi:10.2514/3.10005
- Idan M, 1992, J. Guid. Control Dyn., 15, 901, 10.2514/3.20923 · doi:10.2514/3.20923
- Choi K, 1996, AIAA J., 34, 136, 10.2514/3.13033 · DOI
Cited by
Advances in the Structural Health Monitoring of Bridges Using Piezoelectric Transducers
Chen, Y., & Xue, X. (2018) · Sensors · doi:10.3390/s18124312 · Cited by 87
Metadata
- Authors
- Seydel, R., & Chang, F.-K.
- Venue
- Smart Materials and Structures
- Publisher
- IOP Publishing
- Published
- 2001-04-01
- Volume
- 10
- Issue
- 2
- Pages
- 354-369
- ISSN
- 0964-1726 (ISSN-L)
- 1361-665X
- OpenAlex
- W1998172223
- Cited by
- 167
- References
- 0
- FWCI
- 3.13
- Type
- journal article
- Language
- en
- Open access
- bronze
About these checks
Registry, retraction, Cites and statistics results are computed, not judged, with one exception: a printed reference that no index lists is read once by a model before it counts as a citation error. Claims are extracted by a model and kept only when their quote appears verbatim in the text; each cited source is then checked, with a model’s help, for whether it says what the claim relies on. Those verdicts can be wrong — read the claim’s quote and the cited source before relying on one.
Statistics and arithmetic are recomputed, not judged.
Confidence bands are shown only for fields calibrated on our annotated test set. None is calibrated yet, so no band is shown.
What counts as a claim ›How we measure confidence ›How we check this ›
Are you an author, or do you see a problem with this page? Request a review
How to cite
Cite CoChat for the checks on this page, and the paper for its own findings.
- This page
- CoChat. (2026). Citation check: Impact identification of stiffened composite panels: I. System development. https://app.cochat.ai/papers/10.1088/0964-1726/10/2/323
- The paper
- Seydel, R., & Chang, F.-K. (2001). Impact identification of stiffened composite panels: I. System development. Smart Materials and Structures. https://doi.org/10.1088/0964-1726/10/2/323
Data sources
Bibliographic data: Semantic Scholar, OpenAlex, Crossref.
Contains information from the Semantic Scholar Academic Graph Datasets, made available under the ODC Attribution License (ODC-BY 1.0).
Semantic Scholar’s data is described in: Kinney, R., et al. (2023). The Semantic Scholar Open Data Platform. arXiv:2301.10140.
