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Record W2312350720 · doi:10.2514/6.2006-1254

Comparing Aerodynamic Models for Numerical Simulation of Dynamics and Control of Aircraft

2006· article· en· W2312350720 on OpenAlexfundno aff
Christopher Sequeira, David J. Willis, J. Peraire

Bibliographic record

Venue44th AIAA Aerospace Sciences Meeting and Exhibit · 2006
Typearticle
Languageen
FieldEngineering
TopicComputational Fluid Dynamics and Aerodynamics
Canadian institutionsnot available
FundersNatural Sciences and Engineering Research Council of Canada
KeywordsAerodynamicsAerodynamic forceVortexVorticityComputational fluid dynamicsMechanicsLongitudinal static stabilityReduced frequencyAerospace engineeringControl theory (sociology)PhysicsEngineeringComputer scienceReynolds numberTurbulence

Abstract

fetched live from OpenAlex

Stability and control derivatives are routinely used in the design and simulation of aircraft, yet other aerodynamics models exist that can provide more accurate results for certain simulations without a large increase in computational time. In this paper, several aerodynamics models of varying fidelity are coupled with a six degrees of freedom rigid body dynamics simulation tool to model various geometries under a number of different initial conditions. The aerodynamics models considered are: stability derivatives, strip theory methods, quasi-steady vortex lattice methods, and unsteady panel methods. Through dynamic simulations using a virtual wind tunnel, differences between the various aerodynamics models are examined. The simulations that were examined were primarily concerned with the short period mode in the longitudinal direction. Initial examinations were performed on single-surface geometries and showed good agreement between all models. The follow-up simulations of conventionaland canard-type aircraft configurations showed variations due primarily to the inclusion of a wake model for domain vorticity in the vortex lattice and unsteady panel methods. Although dynamics are considered, the simulations performed did not show unsteady aerodynamics effects causing significant differences in short-period responses. This suggests that the quasi-steady approaches traditionally considered are adequate for the majority of stability and control simulations. The use of unsteady panel methods is only required when reduced frequencies increase to the point where Theodorsen’s lag function contributes significantly to the aerodynamic behavior. This would be the case for high frequency forced flapping flight, but is generally not the case for aircraft.

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.

How this classification was reachedexpand

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 score0.421
Threshold uncertainty score0.610

Codex and Gemma teacher scores by category

CategoryCodexGemma
Metaresearch0.0000.000
Meta-epidemiology (narrow)0.0000.000
Meta-epidemiology (broad)0.0000.000
Bibliometrics0.0000.000
Science and technology studies0.0000.000
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 head0.010
GPT teacher head0.223
Teacher spread0.213 · 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

Classification

machine, unvalidated

Machine predicted; a candidate call from one teacher head, not a consensus.

The models applied no category: nothing in the taxonomy fit this work.
Study designSimulation or modeling
Domainnot available
GenreEmpirical

How this classification was reached, model by model and score by score, is at the end of the page under "How this classification was reached".

Quick stats

Citations31
Published2006
Admission routes1
Has abstractyes

Explore more

Same venue44th AIAA Aerospace Sciences Meeting and ExhibitSame topicComputational Fluid Dynamics and AerodynamicsFrench-language works237,207