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...

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Detalles Bibliográficos
Autores principales: Singh, Prakash, Trivedi, Sharad, Menezes, Viren, Hosseini, Hamid
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Hindawi Publishing Corporation 2014
Materias:
Research Article
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

Internet

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

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