This report describes the computer code and the models developed to form the computer code used to analyze low frequency augmentor instability (rumble). Rumble occurs mainly at high fuel-air ratios and at flight Mach numbers and altitudes were low duct inlet air temperatures and pressures exist. Complete description of the models and the program responsible for their development is contained in AFWAL-TR-81-2113. (Author)
Augmentor Stability Management Program User's Manual
1981
114 pages
Report
No indication
English
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