izpis_h1_title_alt

Analiza sil pri vzletu jadralnega letala s pomočjo vitla
ID Munda, Žiga (Author), ID Grebenšek, Andrej (Mentor) More about this mentor... This link opens in a new window, ID Kosel, Tadej (Comentor)

.pdfPDF - Presentation file, Download (8,47 MB)
MD5: D0D77FA0AA1ED35BF26AD58BEBFA1D79

Abstract
V diplomskem delu je obravnavan vzlet jadralnega letala s pomočjo vitla. Višina, ki jo jadralno letalo lahko doseže, je odvisna od dolžine razvite vrvi in moči pogonskega motorja vitla, vendar pa ta višina ni neskončna. Dolžino vrvi in silo s katero vlečemo letalo omejujeta tako masa vrvi, kot tudi varnostni člen na vrvi, ki varuje jadralno letalo pred preobremenitvijo. Zanima nas do katere mere se še splača povečevati dolžino vlečne vrvi in vlečno silo vitla, da še lahko izvedemo vleko jadralnega letala znotraj omejitev predpisanih v pilotskem priročniku letala.

Language:Slovenian
Keywords:jadralno letalo, vzlet, kot vzpenjanja, drsno razmerje, aeroprofil, vzgon, upor, vitel
Work type:Bachelor thesis/paper
Typology:2.11 - Undergraduate Thesis
Organization:FS - Faculty of Mechanical Engineering
Place of publishing:Ljubljana
Publisher:[Ž. Munda]
Year:2020
Number of pages:XXII, 48 str.
PID:20.500.12556/RUL-116051 This link opens in a new window
UDC:629.734.33:533.6(043.2)
COBISS.SI-ID:16693251 This link opens in a new window
Publication date in RUL:09.05.2020
Views:1523
Downloads:300
Metadata:XML DC-XML DC-RDF
:
Copy citation
Share:Bookmark and Share

Secondary language

Language:English
Title:Analysis of forces during glider winch launch
Abstract:
The diploma thesis deals with glider winch launch. Hight, which glider can reach depends on tow cable length and the towing force of winch, but only to some extent. Length of tow rope and towing force are limited by cable mass and by strength of weak link, this will break before any damage can be done to the glider by overstressing it. Goal of this thesis is to analyze up to what extent is viable to extend tow cable length and increase towing force of winch for achieving greatest launch height, but still to remain inside limitations prescribed in flight manual of a glider.

Keywords:glider, take off, angle of climb, glide ratio, aerofoil, lift, drag, winch

Similar documents

Similar works from RUL:
Similar works from other Slovenian collections:

Back