Artikel

Simulasi fasa II even penerbangan roket air dengan prediktor iteratif berbasis matlab

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SIGMA, JURNAL SAINS DAN TEKNOLOGI, Vol. 13, No. 1 Januari 2010, ABSTRAK : An event iterative prediktor for water rocket filigt was developed using MATLAB. This proposed prediktor can be used to solve the problem of phase II as well as strutz performend on spereadsheet. It uses variation of spesific mass as the consequence of the compression. Using the initial temperature are 20 derajad C and 25 derajad C in shootinger model, it needs 0.06 sec to finish the phase Ii whice enhances accurary of the prediction is 20 %. It also shows that the temperature bdecrease when the fluid in water rocket expanding.

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Ketersediaan

Informasi Detail

Judul Seri

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No. Panggil

JURNAL

Penerbit

Yogyakarta : Universitas Sanata Dharma - LPPM., 2010

Deskripsi Fisik

Hal. 29-35., ilus.; 29 cm.; Hal. 35

Bahasa

Indonesia

ISBN/ISSN

1410-5888

Klasifikasi

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Tipe Isi

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Tipe Media

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Tipe Pembawa

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Edisi

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Subjek

MATLAB
WATER ROCKET
PHASE II

Info Detail Spesifik

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Pernyataan Tanggungjawab

PRASETYADI,A

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