Drag and rolling moment measurements using accelerometer-based force balance in a shock tunnel
Author:
Funder
Agency for Defense Development
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Link
https://link.springer.com/content/pdf/10.1007/s00193-023-01143-4.pdf
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4. Kim, K., Park, G., Jin, S.: Flameholding characteristics of ethylene-fueled model scramjet in shock tunnel. Acta Astronaut. 161, 446–464 (2019). https://doi.org/10.1016/j.actaastro.2019.02.022
5. Ewald, B.F.R.: Multi-component force balances for conventional and cryogenic wind tunnels. Meas. Sci. Technol. 11(6), 81–94 (2000). https://doi.org/10.1088/0957-0233/11/6/201
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