This document presents the results from the application of PITAP procedure to two typical aircraft configurations. The two configurations used are the Lightweight Fighter (LWF) and the F-4J. The Lightweight Fighter in the example is a study configuration for which extensive analysis and wind tunnel test data are available for comparison with predicted results. The F-4J is also a configuration that has been extensively tested during the Exhaust System Interaction Program. Data from these tests are used to compare with PITAP predicted results.


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