Hirotaka Sakaue

Prof. Hirotaka Sakaue

University of Notre Dame
orcid

Research Focus & Metrics

Academic Career Length

27Years (2000-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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3 January 2014 in Annual Review of Fluid Mechanics
Verified
Journal Article
Closed access
JGJames Gregory
James Gregory
Hirotaka SakaueHirotaka Sakaue
Hirotaka Sakaue
TLTianshu Liu
Tianshu Liu
JSJohn P. Sullivan
John P. Sullivan
The development and capabilities of fast-responding pressure-sensitive paint (fast PSP) are reviewed within the context of recent applications to aerodynamic and acoustic investigations. PSP is an optical technique for determining surface pressure distributions by measuring changes in the intensity of emitted light, whereas fast PSP is an extension applicable to unsteady flows and acoustics. Most fast PSP formulations are based on the development of porous binders that allow for rapid oxygen diffusion and interaction with the chemical sensor. This article reviews the development of porous binders, the selection of luminophore molecules suitable for unsteady testing, dynamic calibrations of PSP, data-acquisition methods, and noteworthy applications for flow and acoustic diagnostics. Calibrations of the dynamic response of fast PSP show a flat frequency response to at least 6 kHz, with some paint formulations exceeding a response of 1 MHz. Various applications of fast PSP are discussed that highlight the capabilities of the technique, and concluding remarks highlight the need for the future development of fast PSP.

10 May 2023 in Nature
Verified
Journal Article
Open access
PDF file
MZMinxiang Zeng
Minxiang Zeng
YDYipu Du
Yipu Du
QJQiang Jiang
Qiang Jiang
NKNicholas Kempf
Nicholas Kempf
CWChen Wei
Chen Wei
YZYanliang Zhang
Yanliang Zhang
The development of new materials and their compositional and microstructural optimization are essential in regard to next-generation technologies such as clean energy and environmental sustainability. However, materials discovery and optimization have been a frustratingly slow process. The Edisonian trial-and-error process is time consuming and resource inefficient, particularly when contrasted with vast materials design spaces1. Whereas traditional combinatorial deposition methods can generate material libraries2,3, these suffer from limited material options and inability to leverage major breakthroughs in nanomaterial synthesis. Here we report a high-throughput combinatorial printing method capable of fabricating materials with compositional gradients at microscale spatial resolution. In situ mixing and printing in the aerosol phase allows instantaneous tuning of the mixing ratio of a broad range of materials on the fly, which is an important feature unobtainable in conventional multimaterials printing using feedstocks in liquid–liquid or solid–solid phases4–6. We demonstrate a variety of high-throughput printing strategies and applications in combinatorial doping, functional grading and chemical reaction, enabling materials exploration of doped chalcogenides and compositionally graded materials with gradient properties. The ability to combine the top-down design freedom of additive manufacturing with bottom-up control over local material compositions promises the development of compositionally complex materials inaccessible via conventional manufacturing approaches.

14 July 2021 in Aerospace
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Journal Article
Open access
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MYMasafumi Yamazaki
Masafumi Yamazaki
AJAleksandar Jemcov
Aleksandar Jemcov
Hirotaka SakaueHirotaka Sakaue
Hirotaka Sakaue
Icing on an aircraft is the cause of numerous adverse effects on aerodynamic performance. Although the issue was recognized in the 1920s, the icing problem is still an area of ongoing research due to the complexity of the icing phenomena. This review article aims to summarize current research on aircraft icing in two fundamental topics: icing physics and icing mitigation techniques. The icing physics focuses on fixed wings, rotors, and engines severely impacted by icing. The study of engine icing has recently become focused on ice-crystal icing. Icing mitigation techniques reviewed are based on active, passive, and hybrid methods. The active mitigation techniques include those based on thermal and mechanical methods, which are currently in use on aircraft. The passive mitigation techniques discussed are based on current ongoing studies in chemical coatings. The hybrid mitigation technique is reviewed as a combination of the thermal method (active) and chemical coating (passive) to lower energy consumption.

1 October 2001 in AIAA Journal
Verified
Journal Article
Closed access
Hirotaka SakaueHirotaka Sakaue
Hirotaka Sakaue
JSJohn P. Sullivan
John P. Sullivan

15 November 2005 in Measurement Science and Technology
Verified
Journal Article
Closed access
MKMasaharu Kameda
Masaharu Kameda
TTT Tabei
T Tabei
KNK Nakakita
K Nakakita
Hirotaka SakaueHirotaka Sakaue
Hirotaka Sakaue
KAK Asai
K Asai

4 July 2011 in Sensors
Verified
Journal Article
Open access
PDF file
Hirotaka SakaueHirotaka Sakaue
Hirotaka Sakaue
TKTakuma Kakisako
Takuma Kakisako
HIHitoshi Ishikawa
Hitoshi Ishikawa
A pressure-sensitive paint (PSP) with fast response characteristics that can be sprayed on a test article is studied. This PSP consists of a polymer for spraying and a porous particle for providing the fast response. We controlled the polymer content (%) from 10 to 90% to study its effects on PSP characteristics: the signal level, pressure sensitivity, temperature dependency, and time response. The signal level and temperature dependency shows a peak in the polymer content around 50 to 70%. The pressure sensitivity was fairly constant in the range between 0.8 and 0.9 %/kPa. The time response is improved by lowering the polymer content. The variation of the time response is shown to be on the order of milliseconds to ten seconds. A weight coefficient is introduced to optimize the resultant PSPs. By setting the weight coefficient, we can optimize the PSP for sensing purposes.