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Lempeng pembekah: Perbedaan antara revisi

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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&ndash;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&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).}}


== Pranala luar ==
== Pranala luar ==

Revisi per 15 Maret 2016 21.02

Sebuah pelat Splitter 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 splitter mengalihkan lapisan batas memasuki intake mesin.

Referensi

  • 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

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