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Scoping of an Air Supply Configuration for AFC on a Commercial Transport Airplane High Lift SystemA scoping study is being conducted on the air supply for a microjet-based active flow control (AFC) system on a twin-turbofan commercial transport airplane. Microjets provide circulation control using small surface-normal pneumatic jets located near the trailing edge of a lifting surface such as a wing or flap. When located on the pressure side of the lifting surface they increase the lift, and when located on the suction side they decrease lift. In this study, microjets are considered for installation in the flaps of the high-lift version of the Common Research Model (CRM-HL). An air supply system involving bleed air from the airplane’s auxiliary power unit (APU) plus ram air provides the air to the microjets. A model based on the 1D compressible flow equations is applied to analyze the air supply system configuration and predict the microjet flow rate with the resulting airplane performance changes based on Reynolds-averaged Navier-Stokes modeling of microjets on the CRM-HL. The results of this scoping study are encouraging in that APU air can be used to entrain ram air and thereby increase the AFC mass flow rate to achieve effective lift control and airplane performance enhancement during takeoff and landing.
Document ID
20240000584
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
C P Van Dam
(University of California, Davis Davis, United States)
Seyedeh Sheida Hosseini
(Ames Research Center Mountain View, United States)
Shishir A Pandya
(Ames Research Center Mountain View, United States)
Date Acquired
January 13, 2024
Subject Category
Aeronautics (General)
Meeting Information
Meeting: 34th Congress of the International Council of the Aeronautical Sciences
Location: Florence
Country: IT
Start Date: September 9, 2024
End Date: September 13, 2024
Sponsors: International Council of the Aeronautical Sciences
Funding Number(s)
WBS: 081876.02.01.15.01.01
CONTRACT_GRANT: 80NSSC19K0486
CONTRACT_GRANT: 80NSSC20K0685
CONTRACT_GRANT: 80NSSC21K0473
CONTRACT_GRANT: 0NSSC22K0985
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
Keywords
AATT
ARMD
Takeoff
Landing
Flap
Climb Gradient
Lift-to-Drag Ratio
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