Correction: Physical insight into fuel-air mixing for upstream-fuel-injected scramjets via multi-objective design optimization (Journal of Propulsion and Power, (2015), 31, 6, (1505-1523), 10.2514/1.B35661)

Hideaki Ogawa

doi:10.2514/1.B35661.c1

Correction: Physical insight into fuel-air mixing for upstream-fuel-injected scramjets via multi-objective design optimization (Journal of Propulsion and Power, (2015), 31, 6, (1505-1523), 10.2514/1.B35661)

Research output: Contribution to journal › Comment/debate › peer-review

Abstract

This correction pertains to an error in the expression of the mixing vorticity efficiency defined in Eq. (7) in the original article when it was first published online [http://arc.aiaa.org/doi/abs/10.2514/1.B35661]: The correct expression is (Formula Presented) where the effective injector diameter D must be in the numerator rather than in the denominator according to dimensional analysis. The author regrets this error, while the correct definition was used for the calculation of mixing vorticity efficiency in the study, and so this correction does not affect the results, discussions, or conclusions.

Original language	English
Pages (from-to)	AU4
Journal	Journal of Propulsion and Power
Volume	36
Issue number	6
DOIs	https://doi.org/10.2514/1.B35661.c1
Publication status	Published - 2020
Externally published	Yes

All Science Journal Classification (ASJC) codes

Aerospace Engineering
Fuel Technology
Mechanical Engineering
Space and Planetary Science

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title = "Correction: Physical insight into fuel-air mixing for upstream-fuel-injected scramjets via multi-objective design optimization (Journal of Propulsion and Power, (2015), 31, 6, (1505-1523), 10.2514/1.B35661)",

abstract = "This correction pertains to an error in the expression of the mixing vorticity efficiency defined in Eq. (7) in the original article when it was first published online [http://arc.aiaa.org/doi/abs/10.2514/1.B35661]: The correct expression is (Formula Presented) where the effective injector diameter D must be in the numerator rather than in the denominator according to dimensional analysis. The author regrets this error, while the correct definition was used for the calculation of mixing vorticity efficiency in the study, and so this correction does not affect the results, discussions, or conclusions.",

author = "Hideaki Ogawa",

year = "2020",

doi = "10.2514/1.B35661.c1",

language = "English",

volume = "36",

pages = "AU4",

journal = "Journal of Propulsion and Power",

issn = "0748-4658",

publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

number = "6",

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TY - JOUR

T1 - Correction

T2 - Physical insight into fuel-air mixing for upstream-fuel-injected scramjets via multi-objective design optimization (Journal of Propulsion and Power, (2015), 31, 6, (1505-1523), 10.2514/1.B35661)

AU - Ogawa, Hideaki

PY - 2020

Y1 - 2020

N2 - This correction pertains to an error in the expression of the mixing vorticity efficiency defined in Eq. (7) in the original article when it was first published online [http://arc.aiaa.org/doi/abs/10.2514/1.B35661]: The correct expression is (Formula Presented) where the effective injector diameter D must be in the numerator rather than in the denominator according to dimensional analysis. The author regrets this error, while the correct definition was used for the calculation of mixing vorticity efficiency in the study, and so this correction does not affect the results, discussions, or conclusions.

AB - This correction pertains to an error in the expression of the mixing vorticity efficiency defined in Eq. (7) in the original article when it was first published online [http://arc.aiaa.org/doi/abs/10.2514/1.B35661]: The correct expression is (Formula Presented) where the effective injector diameter D must be in the numerator rather than in the denominator according to dimensional analysis. The author regrets this error, while the correct definition was used for the calculation of mixing vorticity efficiency in the study, and so this correction does not affect the results, discussions, or conclusions.

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DO - 10.2514/1.B35661.c1

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AN - SCOPUS:85095131902

SN - 0748-4658

VL - 36

SP - AU4

JO - Journal of Propulsion and Power

JF - Journal of Propulsion and Power

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ER -

Correction: Physical insight into fuel-air mixing for upstream-fuel-injected scramjets via multi-objective design optimization (Journal of Propulsion and Power, (2015), 31, 6, (1505-1523), 10.2514/1.B35661)

Abstract

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