Drag Bookkeeping Strategies for Conventional and Unconventional Nozzles

Alister Simpson; Marco Geron

Drag Bookkeeping Strategies for Conventional and Unconventional Nozzles

Alister Simpson, Marco Geron

School of Mechanical and Aerospace Engineering

Research output: Contribution to conference › Poster › peer-review

Abstract

This presentationinvestigates the development of a coherent and robust methodology for drag bookkeeping strategies considering conventional and adaptive area nozzles. The methodology is developed through the use of 3D RANS simulations of the Dual Flow Separate Reference Nozzle, and of two alternative adaptive nozzle area nozzle geometries developed under the AvAUNT project (EU Clean Sky 2). The methodology investigates the possibility to develop consistent drag bookkeeping strategies considering only limited data availability representative of wind tunnel testing.

Original language	English
Publication status	Published - 02 Aug 2021
Event	AIAA Propulsion & Energy Forum - Online Duration: 09 Aug 2021 → 11 Aug 2021 Conference number: 2021 https://www.aiaa.org/propulsionenergy/

Conference

Conference	AIAA Propulsion & Energy Forum
Period	09/08/2021 → 11/08/2021
Internet address	https://www.aiaa.org/propulsionenergy/

Keywords

CFD
Engine performance
INTEGRATION

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

Cite this

@conference{6ef20d0969794d1d91d576709570c314,

title = "Drag Bookkeeping Strategies for Conventional and Unconventional Nozzles",

abstract = "This presentationinvestigates the development of a coherent and robust methodology for drag bookkeeping strategies considering conventional and adaptive area nozzles. The methodology is developed through the use of 3D RANS simulations of the Dual Flow Separate Reference Nozzle, and of two alternative adaptive nozzle area nozzle geometries developed under the AvAUNT project (EU Clean Sky 2). The methodology investigates the possibility to develop consistent drag bookkeeping strategies considering only limited data availability representative of wind tunnel testing. ",

keywords = "CFD, Engine performance, INTEGRATION",

author = "Alister Simpson and Marco Geron",

year = "2021",

month = aug,

day = "2",

language = "English",

note = "AIAA Propulsion & Energy Forum ; Conference date: 09-08-2021 Through 11-08-2021",

url = "https://www.aiaa.org/propulsionenergy/",

}

TY - CONF

T1 - Drag Bookkeeping Strategies for Conventional and Unconventional Nozzles

AU - Simpson, Alister

AU - Geron, Marco

N1 - Conference code: 2021

PY - 2021/8/2

Y1 - 2021/8/2

N2 - This presentationinvestigates the development of a coherent and robust methodology for drag bookkeeping strategies considering conventional and adaptive area nozzles. The methodology is developed through the use of 3D RANS simulations of the Dual Flow Separate Reference Nozzle, and of two alternative adaptive nozzle area nozzle geometries developed under the AvAUNT project (EU Clean Sky 2). The methodology investigates the possibility to develop consistent drag bookkeeping strategies considering only limited data availability representative of wind tunnel testing.

AB - This presentationinvestigates the development of a coherent and robust methodology for drag bookkeeping strategies considering conventional and adaptive area nozzles. The methodology is developed through the use of 3D RANS simulations of the Dual Flow Separate Reference Nozzle, and of two alternative adaptive nozzle area nozzle geometries developed under the AvAUNT project (EU Clean Sky 2). The methodology investigates the possibility to develop consistent drag bookkeeping strategies considering only limited data availability representative of wind tunnel testing.

KW - CFD

KW - Engine performance

KW - INTEGRATION

M3 - Poster

T2 - AIAA Propulsion & Energy Forum

Y2 - 9 August 2021 through 11 August 2021

ER -

Drag Bookkeeping Strategies for Conventional and Unconventional Nozzles

Abstract

Conference

Keywords

UN SDGs

Fingerprint

Cite this