NASA Technical Reports Server (NASA) · 1982 · 10 citations · 0 references
EngineeringAerospace EngineeringMechanical EngineeringAerospace StructuresAircraft DesignFlight MechanicsAircraft PerformanceEngine DesignEngine DiagnosticsEngine PerformanceEngine TestingLoad AnalysisAircraft Performance DegradationBlade Tip ClearanceEngine Load CharacterizationFlight ConditionsFlight LoadsFlight Test Performance EvaluationPerformance DegradationPerformance Deterioration Modeling
Flight loads on the 747 propulsion system and resulting JT9D blade to outer airseal running clearances during representative acceptance flight and revenue flight sequences were measured. The resulting rub induced clearance changes, and engine performance changes were then analyzed to validate and refine the JT9D-7A short term performance deterioration model.