Full-Carpet Design of a Low-Boom Demonstrator ConceptThe Cart3D adjoint-based design framework is used to mitigate the undesirable o -track sonic boom properties of a demonstrator concept designed for low-boom directly under the flight path. First, the requirements of a Cart3D design mesh are determined using a high-fidelity mesh adapted to minimize the discretization error of the CFD analysis. Low-boom equivalent area targets are then generated at the under-track and one off-track azimuthal position for the baseline configuration. The under-track target is generated using a trim- feasible low-boom target generation process, ensuring that the final design is not only low-boom, but also trimmed at the specified flight condition. The o -track equivalent area target is generated by minimizing the A-weighted loudness using an efficient adjoint-based approach. The configuration outer mold line is then parameterized and optimized to match the off-body pressure distributions prescribed by the low-boom targets. The numerical optimizer uses design gradients which are calculated using the Cart3D adjoint- based design capability. Optimization constraints are placed on the geometry to satisfy structural feasibility. The low-boom properties of the final design are verified using the adaptive meshing approach. This analysis quantifies the error associated with the CFD mesh that is used for design. Finally, an alternate mesh construction and target positioning approach offering greater computational efficiency is demonstrated and verified.
Document ID
20160005991
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Ordaz, Irian (NASA Langley Research Center Hampton, VA, United States)
Wintzer, Mathias (Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Rallabhandi, Sriram K. (National Inst. of Aerospace Hampton, VA, United States)
Date Acquired
May 10, 2016
Publication Date
June 22, 2015
Subject Category
Aerodynamics
Report/Patent Number
NF1676L-19992Report Number: NF1676L-19992
Meeting Information
Meeting: AIAA Applied Aerodynamics Conference
Location: Dallas, TX
Country: United States
Start Date: June 22, 2015
End Date: June 26, 2015
Sponsors: American Inst. of Aeronautics and Astronautics