Wing/Store Flow-Field Measurement at Transonic Speeds Using a Laser Velocimeter

Transonic Wing/Store Flow-Field Measurement Using a Laser Velocimeter

“…As shown in Table 1 each configuration was tested at M** = 0.920, which was determined experimentally (Ref. 2) as the lowest Mach number for which a shock was firmly established between the store and the wing lower surface of Configuration 201. In addition, selected configurations were tested at M,, = 0.975 and/or 1.025.…”