1. AIAA 2003 Calibration and use of internal strain gauge balances with application to wind tunnel testing R-091-2003 American Institute of Aeronautics and Astronautics (AIAA) Reston, Virginia
2. David , G. 1989 Wind tunnel support system effects on a fighter aircraft model at Mach numbers from 0.6 to 2.0 AEDC-TR-89-4(ADA210614) Arnold Engineering Development Center Tennessee