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Record W4412055717 · doi:10.1016/j.ast.2025.110565

Aerodynamic shape optimization of a supersonic transport including a subsonic static margin constraint

2025· article· en· W4412055717 on OpenAlex
Sabet Seraj, Anıl Yıldırım, Joaquim R. R. A. Martins

Why this work is in the frame

A frame that forgets how it found something cannot be audited. These are the routes that admitted this work.

fundA Canadian funder is recorded on the work.
no affNo Canadian affiliation: this work is invisible to an affiliation-only frame.
No Canadian affiliation. An affiliation-only frame, the usual design, would never have seen this work. It is one of the works that make the case for inverting the frame.

Bibliographic record

VenueAerospace Science and Technology · 2025
Typearticle
Languageen
FieldEngineering
TopicComputational Fluid Dynamics and Aerodynamics
Canadian institutionsnot available
FundersNatural Sciences and Engineering Research Council of CanadaLangley Research CenterNational Aeronautics and Space Administration
KeywordsSupersonic speedAerodynamicsAerospace engineeringConstraint (computer-aided design)Margin (machine learning)MechanicsPhysicsChoked flowStructural engineeringComputer scienceEngineeringMechanical engineering

Abstract

fetched live from OpenAlex

Designing supersonic transport aircraft requires accounting for performance and stability at high-speed and low-speed conditions. Previous work demonstrated that there is a trade-off between high-speed performance and low-speed stability. Numerical optimization presents the opportunity to obtain the best high-speed performance while requiring stability at low speeds. We perform RANS-based aerodynamic shape optimization with a component-based geometry parameterization approach that enables the optimization of a three-surface supersonic transport configuration. We minimize drag at a supersonic cruise condition with and without a constraint on subsonic pitch stability. The stability constraint enforces a target static margin at a subsonic takeoff condition. The stable optimized designs use larger leading-edge flap deflections at the subsonic condition and have thicker wings. The thicker wings increase the supersonic drag by 0.5% for neutral stability and 0.85% for a 10% static margin. These results demonstrate that aerodynamic shape optimization is a valuable tool for designing supersonic transport aircraft accounting for supersonic performance and subsonic stability.

Fetched live from OpenAlex and de-inverted. Abstracts are not stored in this database: the inverted indexes are 8.6 GB of the frame’s 9.3 GB of text, and the host has 13 GB free.

Full frame distilled prediction

Teacher imitation

Not calibrated prevalence, not ground truth. Human validation pending. Learned from the 10,348 direct Codex labels and 10,348 direct Gemma labels. Candidate is the union of thresholded teacher heads; consensus is their intersection. These outputs are machine_predicted_unvalidated and are not human labels or direct frontier model labels.

metaresearch head score (Codex)0.000
metaresearch head score (Gemma)0.000
Version: codex-gemma-dda1882f352aValidation status: machine_predicted_unvalidated
Candidate categoriesnone
Consensus categoriesnone
DomainCandidate signal: none · Consensus signal: none
Study designCandidate signal: Simulation or modeling · Consensus signal: Simulation or modeling
GenreCandidate signal: Empirical · Consensus signal: Empirical
Teacher disagreement score0.410
Threshold uncertainty score0.545

Codex and Gemma teacher scores by category

CategoryCodexGemma
Metaresearch0.0000.000
Meta-epidemiology (narrow)0.0000.000
Meta-epidemiology (broad)0.0000.000
Bibliometrics0.0010.002
Science and technology studies0.0000.001
Scholarly communication0.0000.000
Open science0.0000.000
Research integrity0.0000.000
Insufficient payload (model declined to judge)0.0000.000

Machine scores (provisional)

The two teacher heads of the student model, read on this work. A score orders the frame for review; it never asserts a category, and the validation status ships verbatim with every row.

Baseline scores from an immature model (maturity gate not passed, 7 training rounds). Scores rank; they never assert a category.

Opus teacher head0.005
GPT teacher head0.220
Teacher spread0.215 · how far apart the two teachers sit on this one work
Validation statusscore_only:v0-immature-baseline · verbatim from the scoring run: score_only means the number may rank works, and no category label ships from it