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Supersonic Configurations at Low Speeds (SCALOS): Wind Tunnel Tests at the University of Washington-an Overview and Some Key Insights
A substantial effort was dedicated, as a part of the NASA funded SCALOS project, to low-
speed wind tunnel testing of multiple configurations at the University of Washington's Kirsten …
speed wind tunnel testing of multiple configurations at the University of Washington's Kirsten …
Supersonic Configurations at Low Speeds (SCALOS): Progress at the University of Washington
This paper highlights extensive wind tunnel testing conducted at the University of Washing-
ton's Kirsten Wind Tunnel during 2023 to support the continuing NASA-sponsored SCALOS …
ton's Kirsten Wind Tunnel during 2023 to support the continuing NASA-sponsored SCALOS …
The Impact of Vortex Breakdown on the Longitudinal Flight Behavior of the SCALOS Aircraft
Designing and certifying the next generation of commercial supersonic vehicles is a
complex process. Typically, the aerodynamic design of lifting surfaces is optimized for cruise …
complex process. Typically, the aerodynamic design of lifting surfaces is optimized for cruise …
Supersonic Configurations at Low Speeds (SCALOS): Correlation of CFD and Wind Tunnel Test Results
STAR-CCM+ RANS CFD modeling is used to simulate low-speed wind tunnel tests of
configurations studied by the NASA-funded SCALOS project (Supersonic Configurations at …
configurations studied by the NASA-funded SCALOS project (Supersonic Configurations at …
Performance Evaluation of a Graph Neural Network-Augmented Multi-Fidelity Workflow for Predicting Aerodynamic Coefficients on Delta Wings at Low Speed
Conceptual design of a stable and efficient supersonic transport (SST) aircraft during takeoff
and landing, where higher angle-of-attack (AOA) induces complex aerodynamic …
and landing, where higher angle-of-attack (AOA) induces complex aerodynamic …
Controller Agnostic Design Metrics for Stochastic Disturbance Rejection
This paper presents a framework to compute the probabilities and the expected frequencies
of exceedance of design limits by the outputs and inputs of a linear system driven by …
of exceedance of design limits by the outputs and inputs of a linear system driven by …
Aerodynamic Design Optimization of a Supersonic Transport Aircraft Considering Low-Speed Stability
S Seraj - 2024 - deepblue.lib.umich.edu
Designing supersonic transport (SST) aircraft requires accounting for performance and
stability at high-speed and low-speed conditions. Previous work demonstrated that there is a …
stability at high-speed and low-speed conditions. Previous work demonstrated that there is a …
Supersonic Configurations at Low Speeds (SCALOS) Lateral-Directional Aerodynamics: Configuration Variations and Control Surface Effects
The NASA-funded SCALOS project has been focusing on the low-speed characteristics of
advanced long-range supersonic configurations. A substantial configuration design space …
advanced long-range supersonic configurations. A substantial configuration design space …
Control Related Metrics for Multidisciplinary Design Optimization
B Bahia Monteiro - 2024 - deepblue.lib.umich.edu
The push for cleaner aviation to meet the net-zero carbon emissions by 2050 goal will
require introducing innovative technologies in future aircraft. Active control is a key enabler …
require introducing innovative technologies in future aircraft. Active control is a key enabler …
Tare & Interference Corrections for Commercial Supersonic Configurations Tested at the University of Washington's Kirsten Wind Tunnel
The unique geometric features of the Supersonic Configurations at Low Speeds (SCALOS)
models that were tested for their aerodynamic characteristics at the University of …
models that were tested for their aerodynamic characteristics at the University of …