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.
Propulsion System Installation Corrections. Volume III Sample Cases
1972
91 pages
Report
No indication
English
Jet & Gas Turbine Engines , Aircraft , Computer Hardware , Turbojet engines , Jet fighters , Performance(Engineering) , Computer programs , Installation , Predictions , Corrections , Afterbodies , Engine air systems components , Exhaust nozzles , Drag , Subsonic flow , Supersonic flow , F-4j aircraft , Boattail drag , F-4 aircraft , J-79-ge-10 engines , Lightweight fighters , Lwf(Lightweight fighters) , Pitap(Propulsion installation and table assembly pro) , Propulsion installation and table assembly program