Aerodynamic performance of bypass engine with nozzle exit area change by warped chevrons

Research output: Contribution to journal › Article › peer-review

Original language	English
Pages (from-to)	731-743
Journal	Journal Of Aerospace Engineering - Part G
Volume	224
Issue number	6
DOIs	https://doi.org/10.1243/09544100JAERO529
Publication status	Published - Jun 2010

Keywords

@article{e4c2ac0c4c4b4c338966bb2e846fa23d,

title = "Aerodynamic performance of bypass engine with nozzle exit area change by warped chevrons",

keywords = "Mechanical, aeronautical and manufacturing engineering",

author = "B Sloan and J Wang and S Spence and S Raghunathan and D Riordan",

year = "2010",

month = jun,

doi = "10.1243/09544100JAERO529",

language = "English",

volume = "224",

pages = "731--743",

journal = "Journal Of Aerospace Engineering - Part G",

issn = "0954-4100",

publisher = "SAGE Publications Ltd",

number = "6",

}

TY - JOUR

T1 - Aerodynamic performance of bypass engine with nozzle exit area change by warped chevrons

AU - Sloan, B

AU - Wang, J

AU - Spence, S

AU - Raghunathan, S

AU - Riordan, D

PY - 2010/6

Y1 - 2010/6

KW - Mechanical, aeronautical and manufacturing engineering

U2 - 10.1243/09544100JAERO529

DO - 10.1243/09544100JAERO529

M3 - Article

SN - 0954-4100

VL - 224

SP - 731

EP - 743

JO - Journal Of Aerospace Engineering - Part G

JF - Journal Of Aerospace Engineering - Part G

IS - 6

ER -