Research Article

Dynamic Calibration and Validation of an Accelerometer Force Balance for Hypersonic Lifting Models

Table 1

Freestream conditions for tests in tunnel.

Test gas Pressure
(Pa)
Temperature
(K)
Mach no. Total enthalpy
(MJ/kg)
Reynolds no.
(/m)

Air 50.6 55.4 8 0.768
( ) ±3.74% ±3.74% ±0.25% ±3.74% ±3.63%