Correction: Design and Numerical Investigation of a Hypersonic Waverider based Entry, Descent, and Landing Architecture Assisted by Supersonic Retro-Propulsion(26th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, ADSTCS 2022, (2022), 10.2514/6.2022-2734)

Debdoot Ghosh; Hideaki Ogawa

doi:10.2514/6.2022-2734.c1

Correction: Design and Numerical Investigation of a Hypersonic Waverider based Entry, Descent, and Landing Architecture Assisted by Supersonic Retro-Propulsion(26th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, ADSTCS 2022, (2022), 10.2514/6.2022-2734)

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

Abstract

Correction Notice The first sentence in the second paragraph of the conclusion should read that the time taken by the waverider to reach a suitable velocity to perform SRP is 23.33 minutes, not 23.3 seconds.

Original language	English
Journal	26th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, ADSTCS 2022
DOIs	https://doi.org/10.2514/6.2022-2734.c1
Publication status	Published - 2022
Externally published	Yes
Event	26th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, ADSTCS 2022 - Toulouse, France Duration: May 16 2022 → May 19 2022

All Science Journal Classification (ASJC) codes

Aerospace Engineering
Electrical and Electronic Engineering
Mechanical Engineering

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Ghosh, D., & Ogawa, H. (2022). Correction: Design and Numerical Investigation of a Hypersonic Waverider based Entry, Descent, and Landing Architecture Assisted by Supersonic Retro-Propulsion(26th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, ADSTCS 2022, (2022), 10.2514/6.2022-2734). 26th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, ADSTCS 2022. https://doi.org/10.2514/6.2022-2734.c1

Correction: Design and Numerical Investigation of a Hypersonic Waverider based Entry, Descent, and Landing Architecture Assisted by Supersonic Retro-Propulsion(26th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, ADSTCS 2022, (2022), 10.2514/6.2022-2734). / Ghosh, Debdoot; Ogawa, Hideaki.
In: 26th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, ADSTCS 2022, 2022.

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

Ghosh, D & Ogawa, H 2022, 'Correction: Design and Numerical Investigation of a Hypersonic Waverider based Entry, Descent, and Landing Architecture Assisted by Supersonic Retro-Propulsion(26th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, ADSTCS 2022, (2022), 10.2514/6.2022-2734)', 26th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, ADSTCS 2022. https://doi.org/10.2514/6.2022-2734.c1

Ghosh D, Ogawa H. Correction: Design and Numerical Investigation of a Hypersonic Waverider based Entry, Descent, and Landing Architecture Assisted by Supersonic Retro-Propulsion(26th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, ADSTCS 2022, (2022), 10.2514/6.2022-2734). 26th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, ADSTCS 2022. 2022. doi: 10.2514/6.2022-2734.c1

Ghosh, Debdoot ; Ogawa, Hideaki. / Correction : Design and Numerical Investigation of a Hypersonic Waverider based Entry, Descent, and Landing Architecture Assisted by Supersonic Retro-Propulsion(26th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, ADSTCS 2022, (2022), 10.2514/6.2022-2734). In: 26th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, ADSTCS 2022. 2022.

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title = "Correction: Design and Numerical Investigation of a Hypersonic Waverider based Entry, Descent, and Landing Architecture Assisted by Supersonic Retro-Propulsion(26th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, ADSTCS 2022, (2022), 10.2514/6.2022-2734)",

abstract = "Correction Notice The first sentence in the second paragraph of the conclusion should read that the time taken by the waverider to reach a suitable velocity to perform SRP is 23.33 minutes, not 23.3 seconds.",

author = "Debdoot Ghosh and Hideaki Ogawa",

note = "Publisher Copyright: {\textcopyright} 2022 by the American Institute of Aeronautics and Astronautics, Inc.; 26th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, ADSTCS 2022 ; Conference date: 16-05-2022 Through 19-05-2022",

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Correction: Design and Numerical Investigation of a Hypersonic Waverider based Entry, Descent, and Landing Architecture Assisted by Supersonic Retro-Propulsion(26th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, ADSTCS 2022, (2022), 10.2514/6.2022-2734)

Abstract

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