Measurement and Analysis of Wing and Tail Buffeting Loads on a Fighter-type Airplane

The buffeting loads measured on the wing and tail of a fighter-type airplane during 194 manuevers are given in tabular form, along with the associated flight conditions. Measurements were made at altitudes of 30,000 to 10,000 feet and at speeds up to a Mach number of 0.8. Least-squares methods have been used for a preliminary analysis of data.