Measurement Technique for Ideal Selection of Sensors and Accurate Force Recovery on Aerodynamic Models
- 30 April 2021
- journal article
- research article
- Published by Springer Science and Business Media LLC in Experimental Techniques
- Vol. 46 (2), 1-12
- https://doi.org/10.1007/s40799-021-00472-2
Abstract
No abstract availableKeywords
This publication has 18 references indexed in Scilit:
- An accelerometer balance for the measurement of roll, lift and drag on a lifting model in a shock tunnelMeasurement Science and Technology, 2011
- Accelerometer-Based Force Balance for High Enthalpy FacilitiesJournal of Aerospace Engineering, 2010
- Three-Component Force Measurements on a Large Scramjet in a Shock TunnelJournal of Spacecraft and Rockets, 2004
- Dynamic calibration of force balances for impulse hypersonic facilitiesShock Waves, 2003
- An accelerometer balance system for measurement of aerodynamic force coefficients over blunt bodies in a hypersonic shock tunnelMeasurement Science and Technology, 2003
- Design, modelling and analysis of a six component force balance for hypervelocity wind tunnel testingComputers & Structures, 2001
- Three-component force balance for flows of millisecond durationAIAA Journal, 1996
- Drag measurements at Mach 5 using a stress wave force balanceExperiments in Fluids, 1995
- Finite element modelling of a three-component force balance for hypersonic flowsComputers & Structures, 1995
- Drag balance for hypervelocity impulse facilitiesAIAA Journal, 1991