Transonic wind tunnel investigation of limit cycle oscillations on fighter type wings - Update

Author:

CUNNINGHAM, JR. ATLEE1,DEN BOER RUUD2

Affiliation:

1. General Dynamics Corp., Fort Worth, TX

2. National Aerospace Laboratory, Amsterdam, Netherlands

Publisher

American Institute of Aeronautics and Astronautics

Reference24 articles.

1. Figure 2 LC0 Configuration (Oscillating

2. The wind tunnel tests were performed using a computer controlled data acquisition system (see Figure 3) called PHARAO (Processor for HArmonic and Random Oscillations), which is capable of sampling 64 (time) signals simultaneously. Using a switch panel in the LC0 test, the process

3. TABLE 2 FREQUENCY/AMPLITUDE TEST MATRIX 1986TEST

4. Steady Pressures at the Wing-Tip Pressure Row for the HST Test and the 1986 Test (Reference 11 - FullWing)

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