Wind tunnel model support and attitude control

Details Wind tunnel model support and attitude control Wind tunnel model support and attitude control

1988-10-14

1990-05-01

Orsino, Joseph A.

Measuring and testing

Wind tunnel: aerodynamic wing and propeller study

G01M 900

Patent

active

049207911

ABSTRACT:
The invention is directed to a model support system for wind tunnel testing. The two embodiments of the model support use a conventual 2-shell strain gauge balance in conjunction with aerodynamically shaped support vanes with one attached to each end of the inner rod (non-metric) of balance with one half below and the other half above the balance.

REFERENCES:
patent: 3276251 (1966-10-01), Reed III
patent: 3695101 (1972-10-01), Hanson
patent: 4116056 (1978-09-01), Bulychev et al.
patent: 4658635 (1987-04-01), Pszolla et al.

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