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Dynamic Calibration and Validation of an Accelerometer Force Balance for Hypersonic Lifting Models
An accelerometer-based force balance was designed and developed for the measurement of drag, lift, and rolling moment on a blunt-nosed, flapped delta wing in a short-duration hypersonic shock tunnel. Calibration and validation of the balance were carried out by a convolution technique using hammer p...
| Autores principales: | , , , |
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| Formato: | Online Artículo Texto |
| Lenguaje: | English |
| Publicado: |
Hindawi Publishing Corporation
2014
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| Materias: | |
| Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC3918397/ https://www.ncbi.nlm.nih.gov/pubmed/24574921 http://dx.doi.org/10.1155/2014/813759 |