Simulasi Fasa II Evan Penerbangan Roket Air dengan Prediktor Iteratif Berbasis Matlab  

Oleh:

Prasetyadi, A.

Jenis: Article from Journal - ilmiah nasional - tidak terakreditasi DIKTI
Dalam koleksi: SIGMA: Jurnal Sains dan teknologi vol. 13 no. 1 (Jan. 2010), page 29-35.
Topik: Water Rocket; Phase II; Simulasi; MATLAB

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Perpustakaan Pusat (Semanggi) Nomor Panggil: SS25 Non-tandon: 1 (dapat dipinjam: 0) Tandon: tidak ada

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Isi artikel

An event iterative predictor for water rocket flight was developed using MATLAB. This proposed predictor can be used to solve the problem of phase II as well as Strutz performed on spreadsheet. It uses variation of specific mass as the consequence of the compression. Using the initial temperature are 20"0C and 25"0C in Shootinger model, it needs 0.06 sec to finish the phase II which enhances accuracy of the prediction is 20%. It also shows that the temperature decrease when the fluid in water rocket expanding.

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