Korelacija podataka iz aerodinamičkog tunela s podacima o letu aviona

undergraduate thesis

• Title (english): Correlation between Wind Tunnel Data and Aircraft Flight Data
• Author: Šime Mitrović
• Mentor: Davor Franjković (mentor)
• Committee member: Karolina Krajček Nikolić (predsjednik povjerenstva)
• Committee member: Anita Domitrović (član povjerenstva)
• Committee member: Ernest Bazijanac (član povjerenstva)
• Granter: University of Zagreb; Faculty of Transport and Traffic Sciences; (Division of Aeronautics); (Department of Aeronautics); Zagreb
• Defense date and country: 2022-09-14, Croatia
• Scientific / art field, discipline and subdiscipline: TECHNICAL SCIENCES; Traffic and Transport Technology

Abstract

Eksperimentalna aerodinamika nastoji dati odgovore na problematiku strujanja fluida preko tijela. Eksperimenti se provode u aerodinamičkim tunelima na temelju izračuna postavljenih preko teorije sličnosti i strujanja. Granični slojevi predstavljaju usko područje uz konturu aeroprofila pod utjecajem viskoznih i tangencijalnih sila. Prilikom testiranja posebna pozornost obraća se na ostvarivanje što izraženije sile uzgona, uz što manje otpore. Upravljačke površine i zanimljive izvedbe kompenzacija predstavljaju znatnu korist eksperimentiranja u svrhu poboljšanja upravljivosti zrakoplova. Stabilnost zrakoplova opisana je kroz gibanja u određenom prostoru.

Abstract (english)

Experimental aerodynamics strives to solve major problems surrounding fluid flow against objects. Experiments are conducted inside of wind tunnels based on calculations derived from similarity of flow theory. Boundary layers represent narrow areas close to contures of aeroprofiles under the influence of viscose and tangential forces. During tests, special focus is set onto achieving as great as possible lift, while reducing drag. Control surfaces and quite interesting solutions of compensations represent great value of commencing of experiments in regard of improving of maneuverability of aircraft. Stability of aircraft is described through set of motions in defined space.

• Keywords: aerotunel; teorija sličnosti; strujanje; granični sloj; upravljačke površine; upravljivost; stabilnost
• Keywords (english): wind tunnel similarity theory; flow; boundary layer; control surfaces; maneuverability; stability
• Language: croatian
• URN:NBN: urn:nbn:hr:119:945217
• 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: 2022-10-06 10:19:17