Izračun performansi jednomotornog zrakoplova s propelerskim pogonom

undergraduate thesis

• Title (english): Performance Calculations of Single Engine Propeller-driven Aircraft
• Author: Domagoj Mandić
• Mentor: Davor Franjković (mentor)
• Committee member: Anita Domitrović (predsjednik povjerenstva)
• Committee member: Tomislav Radišić (član povjerenstva)
• Committee member: Željko Marušić (član povjerenstva)
• Granter: University of Zagreb; Faculty of Transport and Traffic Sciences; (Division of Aeronautics); (Department of Aeronautics); Zagreb
• Defense date and country: 2017-09-12, Croatia
• Scientific / art field, discipline and subdiscipline: TECHNICAL SCIENCES; Traffic and Transport Technology; Air Traffic

Abstract

Performanse predstavljaju specifičnu skupinu mogućnosti i sposobnosti koju određeni zrakoplov posjeduje u rasponu različitih masa i brzina na određenim visinama. Gledano sa stajališta fazi leta, specijalnim performansama se smatraju faze polijetanja, slijetanja i zaokreta zrakoplova. Kroz cjelokupni rad analizirani su osnovni elementi izračuna u pogledu fizikalnih zakona za različite faze leta (horizontalni let, penjanje, spuštanje, polijetanje, slijetanje i zaokreti), a nakon svakog režima leta, kao zasebnog poglavlja. Također, prikazani su proračunati parametri za specifične mase i visine, unutar raspona masa, zrakoplova Beechcraft Bonanza. Prikaz proračunatih parametara, ovisno o fazi leta, prikazani su kroz nekoliko grafikona i tablica. Kroz analiziranu materiju, spominju se i bitni vanjski čimbenici koji pridonose cjelokupnom izračunu performansi, kao i karakteristike zrakoplova poput mase, pogonske grupe, konstruktivnih te aerodinamičkih karakteristika.

Abstract (english)

Performance represent the specific group of capabilities and abilities which some aircraft possess in different span of masses and velocities values at certain altitudes. Viewed from the standpoint of the flight phases: take off, landing and an airplane turn are considered as the special performance. Throughout work, the calculations regarding physical laws for the different flight phases (level flight, climbing, descending, take off, landing and turns), are analyzed as the separate chapter. The calculated parameters of Beechcraft Bonanza, for the different span of masses and altitudes within defined range are shown as well. The calculated parameters review, depending on flight phases, are shown through several charts and tables. Throughout analyzed matter, major external factors are mentioned, which contribute overall performance calculation as well as an aircraft characteristics like mass, powerplant, construction and aerodynamics.

• Keywords: performanse zrakoplova; značajne karakteristike; elementi izračuna; režimi leta
• Keywords (english): aircraft performance; significant features; calculation elements; flight phases
• Language: croatian
• URN:NBN: urn:nbn:hr:119:413384
• Study programme: Title: Aeronautics; Study programme type: university; Study level: undergraduate; Academic / professional title: sveučilišni/a prvostupnik/prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka aeronautike (sveučilišni/a prvostupnik/prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka aeronautike)
• Type of resource: Text
• File origin: Born digital
• Access conditions: Open access
• Created on: 2017-09-19 10:07:02