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Lempeng pembekah: Perbedaan antara revisi

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(6 revisi perantara oleh 6 pengguna tidak ditampilkan)
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{{Underlinked|date=Februari 2023}}
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[[File:Royal Military Museum Brussels 2007 230.JPG|thumb|200px]]
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Sebuah '''pelat Splitter''' adalah komponen di beberapa pesawat bermesin jet, digunakan untuk mengontrol aliran udara ke dalam mesin.


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[[Berkas:Royal Military Museum Brussels 2007 230.JPG|jmpl|200px]]
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Dimana asupan udara mesin dipasang setengah jalan kembali sepanjang badan pesawat atau di bawah sayap, lempeng splitter mengalihkan lapisan batas memasuki intake mesin.
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Sebuah '''lempeng pembekah''' adalah komponen di beberapa pesawat bermesin jet, digunakan untuk mengontrol aliran udara ke dalam mesin.

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Di mana asupan udara mesin dipasang setengah jalan kembali sepanjang badan pesawat atau di bawah sayap, lempeng pembekah mengalihkan lapisan batas memasuki saluran masuk mesin.


== Referensi ==
== Referensi ==
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<!--When citing these in the article remove from here-->
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* {{cite journal |last1=Hughes |first1=Donald L |last2=Holztman |first2=Jon K |last3=Johnson |first3=Harold J|year=1972 |title=Flight-Determined Characteristics of an Air Intake System of an F-111A Airplane |journal=Technical Note|volume=D&ndash;6679 |issue= |pages= |publisher=[[NASA]] |doi= |url=http://www.nasa.gov/centers/dryden/pdf/87801main_H-661.pdf|accessdate=15 February 2013}}
* {{cite journal |last1=Hughes |first1=Donald L |last2=Holztman |first2=Jon K |last3=Johnson |first3=Harold J|year=1972 |title=Flight-Determined Characteristics of an Air Intake System of an F-111A Airplane |journal=Technical Note|volume=D–6679 |issue= |pages= |publisher=[[NASA]] |doi= |url=http://www.nasa.gov/centers/dryden/pdf/87801main_H-661.pdf|accessdate=15 February 2013}}
* {{cite book |last=Hünecke |first=Klaus |authorlink= |title=Jet Engines |url= |accessdate=15&nbsp;February 2013 |year=1997|publisher=Airlife|location=England |isbn=1853108340 |pages=76&ndash;79|quote=... the thickening of the boundary layer that develops at high angles-of-attack along the lower side of the fuselage forebody [in the F-16]. In order to prevent low-energy flow from entering the engine, the intake had to be offset from the fuselage to free it from the boundary layer, which uninterruptedly passes along the fuselage. The intake cowl [of the F-16] features a moderately blunt lower lip that transitions into a sharp leading-edge extension or '''''splitter plate''''' on the upper side (close to the fuselage).}}
* {{cite book|last=Hünecke|first=Klaus|authorlink=|title=Jet Engines|url=|accessdate=15&nbsp;February 2013|year=1997|publisher=Airlife|location=England|isbn=1853108340|pages=76–79|quote=... the thickening of the boundary layer that develops at high angles-of-attack along the lower side of the fuselage forebody [in the F-16]. In order to prevent low-energy flow from entering the engine, the intake had to be offset from the fuselage to free it from the boundary layer, which uninterruptedly passes along the fuselage. The intake cowl [of the F-16] features a moderately blunt lower lip that transitions into a sharp leading-edge extension or '''''splitter plate''''' on the upper side (close to the fuselage).}}


==Pranala luar==
== Pranala luar ==
*[http://sortingoutscience.net/2008/12/30/the-scientific-tourist-53-splitter-plates-and-boundary-layers/ http://sortingoutscience.net/2008/12/30/the-scientific-tourist-53-splitter-plates-and-boundary-layers/]
* [http://sortingoutscience.net/2008/12/30/the-scientific-tourist-53-splitter-plates-and-boundary-layers/ http://sortingoutscience.net/2008/12/30/the-scientific-tourist-53-splitter-plates-and-boundary-layers/] {{Webarchive|url=https://web.archive.org/web/20130512001744/http://sortingoutscience.net/2008/12/30/the-scientific-tourist-53-splitter-plates-and-boundary-layers/ |date=2013-05-12 }}


{{Komponen pesawat terbang}}
{{Komponen pesawat terbang}}
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{{pesawat-stub}}


[[Kategori:Komponen propulsi pesawat terbang]]
[[Kategori:Komponen propulsi pesawat terbang]]


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{{pesawat-stub}}

Revisi terkini sejak 14 Juli 2024 06.09

Sebuah lempeng pembekah adalah komponen di beberapa pesawat bermesin jet, digunakan untuk mengontrol aliran udara ke dalam mesin.

Di mana asupan udara mesin dipasang setengah jalan kembali sepanjang badan pesawat atau di bawah sayap, lempeng pembekah mengalihkan lapisan batas memasuki saluran masuk mesin.

Referensi

[sunting | sunting sumber]
  • Hughes, Donald L; Holztman, Jon K; Johnson, Harold J (1972). "Flight-Determined Characteristics of an Air Intake System of an F-111A Airplane" (PDF). Technical Note. NASA. D–6679. Diakses tanggal 15 February 2013. 
  • Hünecke, Klaus (1997). Jet Engines. England: Airlife. hlm. 76–79. ISBN 1853108340. ... the thickening of the boundary layer that develops at high angles-of-attack along the lower side of the fuselage forebody [in the F-16]. In order to prevent low-energy flow from entering the engine, the intake had to be offset from the fuselage to free it from the boundary layer, which uninterruptedly passes along the fuselage. The intake cowl [of the F-16] features a moderately blunt lower lip that transitions into a sharp leading-edge extension or splitter plate on the upper side (close to the fuselage). 

Pranala luar

[sunting | sunting sumber]


Ikon rintisan

Artikel bertopik pesawat terbang dan penerbangan ini adalah sebuah rintisan. Anda dapat membantu Wikipedia dengan mengembangkannya.

Diperoleh dari "https://wiki-indonesia.club/w/index.php?title=Lempeng_pembekah&oldid=26031076"