Sökning: "saab aerodynamik"

Hittade 5 uppsatser innehållade orden saab aerodynamik.

  1. 1. Design, Modeling and Control of an Octocopter

    Master-uppsats, KTH/Optimeringslära och systemteori

    Författare :Oscar Oscarson; [2015]
    Nyckelord :;

    Sammanfattning : This master’s thesis project from the Department of Mathematics at KTH, Royal Institute of Technology, Stockholm, Sweden was carried out at Saab Dynamics, Linköping, Sweden. In this thesis, an octocopter was studied, which is a multirotor vehicle, a rotorcraft with more than two rotors. LÄS MER

  3. 2. Development of Efficient Methods used for Aft-body Assessment

    Master-uppsats, KTH/Aerodynamik

    Författare :Peter Rosén; [2014]
    Nyckelord :;

    Sammanfattning : This paper presents a Master of Science thesis project, performed at SAAB Aeronautics propulsion division in 2014. A method was developed to implement performance calculations on nozzles and aircraft aft-body’s. LÄS MER

  4. 3. 3D Fuel Tank Models for System Simulation

    Master-uppsats, KTH/Aerodynamik

    Författare :Alexandra Oprea; [2012]
    Nyckelord :;

    Sammanfattning : The purpose of the present master thesis is to optimize the current fuel tank simulations procedure for the next generation of JAS 39 Gripen ghters developed by SAAB AB. The current simulation process involves three dierent steps performed in three dierent computer environments. LÄS MER

  5. 4. Evaluation of a CFD method for estimating aerodynamic loads on external stores on JAS 39 Gripen

    Master-uppsats, Institutionen för fysik

    Författare :Jakob Öhrman; [2011]
    Nyckelord :aerodynamic loads; CFD; computational fluid dynamics; simulation; aircraft; external stores; scaling; Saab Aerosystems; JAS 39 Gripen; aerodynamik; luftlaster; CFD; numerisk strömningsmekanik; simulering; flygplan; yttre utrustning; skalning; Saab Aerosystems; JAS 39 Gripen;

    Sammanfattning : Loads determination for external stores on fighter aircraft is an important task for manufacturers in ensuring the safe operation of their aircraft. Due to the large number of possible store combinations, wind tunnel tests – the primary approach to obtaining loads data – cannot be performed for all configurations. LÄS MER

  7. 5. Development of Body and Viscous Contribution to a Panel Program for Potential Flow Computation : Aero Dynamic Analysis and Preliminary Design Tool

    Magister-uppsats, Institutionen för konstruktions- och produktionsteknik

    Författare :Erik Nordin; [2006]
    Nyckelord :Flygteknik; Aerodynamik; Potentiellströmning; Panelprogram; Kroppsmodell; Gränsskiktsmodell;

    Sammanfattning : The aim of this thesis was to develop a potential flow calculation model which includes computation of flow around aircraft bodies (fuselage, engines) and a boundary layer method which calculates the viscous effects over the aircraft wings. The models developed will be merged with an already existing panel program developed by Saab, Linköping, Sweden. LÄS MER