Shock-wave/boundary-layer interaction at a swept compression corner

Araştırma çıktısı: Dergi yayını › Makale › Hakem

2 Atıf (Scopus)

This study was supported by the UYG-AR Applied Research Center of Istanbul Technical University.

Finansörler
UYG-AR
Istanbul Teknik Üniversitesi

Belgeye Erişim

@article{911b726039024b90abc4de2aecae1e4b,

title = "Shock-wave/boundary-layer interaction at a swept compression corner",

author = "Oktay {\"O}zcan and Kaya, \{M. Orhan\}",

year = "1989",

month = nov,

doi = "10.2514/3.10314",

language = "English",

volume = "27",

pages = "1646--1648",

journal = "AIAA Journal",

issn = "0001-1452",

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

number = "11",

}

TY - JOUR

T1 - Shock-wave/boundary-layer interaction at a swept compression corner

AU - Özcan, Oktay

AU - Kaya, M. Orhan

PY - 1989/11

Y1 - 1989/11

UR - https://www.scopus.com/pages/publications/0024767933

U2 - 10.2514/3.10314

DO - 10.2514/3.10314

M3 - Article

AN - SCOPUS:0024767933

SN - 0001-1452

VL - 27

SP - 1646

EP - 1648

JO - AIAA Journal

JF - AIAA Journal

IS - 11

ER -