MétaCan
Menu
Back to cohort
Record W7116287921 · doi:10.1016/j.ast.2025.111548

Investigating the role of propeller geometry and surface characteristics in UAV ice accretion: An experimental study

2025· article· en· W7116287921 on OpenAlex
Manaf Muhammed, Derek Harvey, Hassan Abbas Khawaja, Muhammad S. Virk, Gelareh Momen

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.

aboutThe title or abstract carries a Canadian signal from the geographic lexicon.
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
TopicIcing and De-icing Technologies
Canadian institutionsnot available
FundersNorges Forskningsråd
KeywordsSurface (topology)PropellerVortexUnmanned surface vehicle

Abstract

fetched live from OpenAlex

A lab based experimental study of atmospheric ice accretion on UAV propellers with different geometric and surface characteristics was conducted to study the ice accretion physics and resultant changes in propeller thrust and electrical power consumption. These experiments were conducted at the Anti-icing Materials International Laboratory (AMIL) Icing Wind Tunnel (IWT) at the Université du Québec à Chicoutimi (UQAC), Canada. The experimental icing conditions are determined in accordance with the 14 CFR Part 29 Appendix C for rotorcraft operating at altitudes below 10,000 feet. In this study the influence of following four geometric parameters and two surface characteristics of UAV propeller on ice accretion is analysed: 1) propeller diameter, 2) propeller pitch, 3) propeller chord length, 4) propeller winglets, 4) propeller surface finish and 6) Icephobic coatings. The analysis of results shows that the change in these features does not significantly impact the nature and shape of ice accretion but mainly influence the surface area affected by ice accretion. The thrust coefficient and electrical power coefficients vary considerably with change in propeller geometric features. The variation in propeller blade surface characteristics has a significant impact on the ice shedding characteristics of UAV propeller blade. Considering the high-power requirements of active ice mitigation techniques for UAV propellers, the results obtained from this study can be employed to develop a passive/hybrid ice mitigation approach and further optimize the geometric parameters of UAV propeller blades for efficient operations in icing conditions.

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: Bench or experimental · Consensus signal: none
GenreCandidate signal: Empirical · Consensus signal: Empirical
Teacher disagreement score0.511
Threshold uncertainty score0.399

Codex and Gemma teacher scores by category

CategoryCodexGemma
Metaresearch0.0000.000
Meta-epidemiology (narrow)0.0000.000
Meta-epidemiology (broad)0.0000.000
Bibliometrics0.0000.002
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 head0.009
GPT teacher head0.247
Teacher spread0.239 · 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