Zobrazeno 1 - 10
of 43
pro vyhledávání: '"Lambda Wing"'
Publikováno v:
Journal of Applied Fluid Mechanics, Vol 17, Iss 6, Pp 1182-1190 (2024)
Unmanned Combat Aerial Vehicles (UCAVs) are designed to be lightweight and compact, which can impact their overall lift and aerodynamic capabilities. This study focuses on enhancing the Coefficient of Lift (CL) by optimising the Back Sweep Angle in t
Externí odkaz:
https://doaj.org/article/9ec0953349a646028ad2ac909c5857bd
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2019, Vol. 91, Issue 8, pp. 1100-1112.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-12-2017-0271
Akademický článek
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Akademický článek
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Autor:
M. Murat Yavuz
Publikováno v:
Special Issue 12: 22nd Thermal Science and Technology Congress; Volume: 6, Issue: 6 282-297
Journal of Thermal Engineering
Journal of Thermal Engineering
It is well known in literature that further stages of flow separation and vortex breakdown around wings can be able to cause stall of wings. These formations must be investigated carefully for new plane types. However, some limited studies are availa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6f0665b0087b31690052201793e5aaf7
https://doi.org/10.18186/thermal.829872
https://doi.org/10.18186/thermal.829872
NUMERICAL INVESTIGATION OF FLOW CHARACTERISTICS OF A NON-SLENDER LAMBDA WING UNMANNED AERIAL VEHICLE
Autor:
SOGUKPİNAR, Haci, CAG, Serkan
Publikováno v:
Volume: 9, Issue: 18 481-490
Adıyaman Üniversitesi Mühendislik Bilimleri Dergisi
Adıyaman Üniversitesi Mühendislik Bilimleri Dergisi
Bu Çalışmada, kiriş uzunluğu c=210 mm, süpürme açısı Λ=51°, kalınlığı 3 mm ve rüzgar yönüne 58° açı ile eğimli hücum kenarına sahip lambda kanadının düşük hızlı aerodinamik performansı nümerik olarak incelenmiştir.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=tubitakulakb::91850c18dfb23d726f2a56168422ffa2
https://dergipark.org.tr/tr/pub/adyumbd/issue/74951/1085034
https://dergipark.org.tr/tr/pub/adyumbd/issue/74951/1085034
Akademický článek
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Publikováno v:
CEAS Aeronautical Journal. 9:417-427
In the Transonic Wind Tunnel Gottingen, pitch oscillations were performed with a Lambda wing to study unsteady pressure distributions of vortex dominated flow including transonic effects. The free stream Mach number was varied between 0.3 and 0.7. Sm
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8c8e25bba07e0f6aeaf950a94023dba8
https://doi.org/10.1007/s13272-018-0293-4
https://doi.org/10.1007/s13272-018-0293-4
Autor:
Martin Rein, Michael Paul
Publikováno v:
Journal of Aircraft. 54:1139-1149
Lambda wing configurations are known to possess challenging flight characteristics at transonic Mach numbers. This study tests various methods for increasing the maneuverability and stability of the SACCON, a generic lambda wing configuration. Severa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::43bc93fcc35cfd976e40cc7e95b38a51
https://doi.org/10.2514/1.c034080
https://doi.org/10.2514/1.c034080
Autor:
Stefan Wiggen
Publikováno v:
Aerospace Science and Technology. 47:396-405
Unsteady pressure distributions at a pitching Lambda wing with 53° sweep angle are described in this paper. The tests with a half wing model with a purely round leading edge were conducted in the Transonic Wind Tunnel Gottingen. The free stream Mach
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::92d550c844cd0b9a3767f3e8ed70816d
https://doi.org/10.1016/j.ast.2015.10.007
https://doi.org/10.1016/j.ast.2015.10.007