טוען...
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...
שמור ב:
| Main Authors: | , , , |
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| פורמט: | Artigo |
| שפה: | Inglês |
| יצא לאור: |
Hindawi Publishing Corporation
2014
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| נושאים: | |
| גישה מקוונת: | https://ncbi.nlm.nih.gov/pmc/articles/PMC3918397/ https://ncbi.nlm.nih.gov/pubmed/24574921 https://ncbi.nlm.nih.govhttp://dx.doi.org/10.1155/2014/813759 |
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