Raportti / Helsingin teknillinen korkeakoulu. Aerodynamiikan laboratorio. Sarja B

contributor

• Teknillinen korkeakoulu
• Teknillinen korkeakoulu. Aerodynamiikan laboratorio

hasPart

• A numerical method for analysis and design of airfoils in subsonic flow
• A numerical method for simulating unsteady flow including solid/fluid interaction
• A six degree-of-freedom trajectory model
• A study of aerodynamic noise generated by Neles ball valves
• A theoretical study of axisymmetric contractions for low-speed wind tunnels
• A theoretical study of the effect of a wavelike surface roughness upon the boundary layer transition
• A three-dimensional multigrid algorithm for the Euler and the thin-layer Navier-Stokes equations
• A vortex panel method for slowly oscillating lifting surfaces at subsonic speeds
• Ali- ja ylisoonista potentiaalivirtausta laskevan paneelimenetelmäohjelman NLRAERO testaus VAX 8600 tietokoneessa
• An application of Roe's flux-difference splitting for [kappa]-[epsilon] turbulence model
• An evaluation of the two-dimensional Euler and Navier-Stokes calculations based on a flux-vector splitting
• An experimental study of the effect of a backward facing step in the flat plate upon the laminar boundary-layer
• Calculation of three-dimensional viscous/inviscid interaction in subsonic flow
• Calculation of transonic laminar and turbulent flow past a delta wing
• Comparison of Euler algorithms for two-dimensional shock calculations
• Computation of boundary layer flow using thin-layer Navier-Stokes equations with flux-vector splitting
• Computational study of GA(W)-1 airfoil near stall
• Computations of viscous flow around the HSVA-1 tanker using two versions of the [kappa] - [omega] turbulence model
• Design of single component airfoils using an inverse boundary element method
• Development of an equation of state for an arbitrary mixture of thermally perfect gases to the FINFLO flow solver
• Differenssimenetelmän sovellutus kitkattoman virtauskentän laskemiseksi tuulitunnelin suuttimessa
• Eräs menetelmä rajakerroksen huomioon ottamiseksi laskettaessa yksinkertaisia siipiä paneelimenetelmällä
• Etureunaltaan pyöreän deltasiiven virtauskentän tutkiminen laskennallisin keinoin
• Evaluation of the ZONA51D program
• FINF2A : a multi-block navier-stokes solver for steady two-dimensional and axisymmetric flows
• FINFLO : a finite-volume based computer program for two-dimensional and axisymmetric compressible flow
• FINFLO : the parallel multi-block flow solver
• FINFLO-virtausratkaisijan soveltuvuudesta siipiprofiilin aerodynamiikan määrittämiseen hidaslentoalueessa, kun kohtauskulma on suuri
• Flux vector splitting in general curvilinear coordinates
• Flux vector splitting of the one-dimensional Euler equations
• Grid generation and processing for FINFLO flow solver
• Handling of grid deformation as well as sinkage and trim of a ship in FINFLO-SHIP
• HUTFLY2, Matlab/Simulink-pohjainen lennonsimulointiohjelmisto
• HUTFLY2, Matlab/Simulink-pohjainen lennonsimulointiohjelmisto
• Implementation of a one-equation turbulence model into the FINFLO flow solver
• Implementation of a time-accurate time-integration scheme to the FINFLO flow solver
• Implementing a Reynolds stress turbulence model in the finflo flow solver
• Implementing an explicit algebraic Reynolds stress model into the three-dimensional FINFLO flow solver
• Katsaus ilmataistelun simulointiin
• Kirjallisuustutkimus flutterilentokokeista
• Kirjallisuustutkimus transsoonisesta flutterianalyysistä
• Kármán-Trefftz profiilin y-koordinaatit ja nopeusjakautuman annetuissa x-koordinaatin kohdissa laskeva tietokoneohjelma KARTRE
• Laajennetun kantoviivateorian yleistyksiä ja tietokoneohjelma LIFLI siiven ja siipirunko-yhdistelmän nostovoimajakauman laskemiseksi
• Laminaarituulitunnelin käyttö kuumalanka-anemometrin kalibrointiin ja turbulenssiasteen mittaus
• Leko-70:n laskusiivekkeellä varustetun siipiprofiilimallin tuulitunnelikokeet
• Menetelmä kokoonpuristumattoman potentiaalivirtauksen laskemiseksi poikkileikkaukseltaan suorakulmion muotoisissa kanavissa
• Modernized MBB Panel Code : user's guide including background theory
• Multigrid solution method for the Euler equations
• Navier-Stokes calculations of an axisymmetric SOC-projectile using a low-Reynolds-number [kappa] - [epsilon] turbulence model
• New two-equation turbulence model for aerodymamics applications
• New two-equation turbulence model for aerodymamics applications
• Numeerinen menetelmä lentokoneen pitkittäisliikkeen laskemiseksi
• Numerical integration of the Navier-Stokes equations for steady flow past a wavelike bulge on a flat plate
• Numerical investigation of the effect of a wavelike surface roughness upon the boundary-layer transition
• Numerical investigations into the base drag of various wedges using the base flow model developed by Mauri Tanner
• Numerical simulation of transonic flow around airfoils at high Reynolds numbers using algebraic turbulence models
• On structured grid generation
• On the solid-wall boundary condition of [omega] in the [kappa] - [omega]-type turbulence models
• Peräpaineen teoreettisesta määrityksestä puristumattomassa ja ylisoonisessa vanavesivirtauksessa
• Perävirtauksen vaikutus ammuksen ilmavastukseen ja lentorataan
• POISS2 : a 2D Poisson smoother of structured grids
• POISS3 : a 3D poisson smoother of structured grids
• Potentiaaliteoreettisen virtauksen laskeminen siivelle ja siipirunkoyhdistelmällä
• Potentiaalivirtauksen nopeusjakautuman ja aerodynaamisten kertoimien laskeminen siipiprofiilille HP-2000 tietokoneella
• Range and endurance of jet-engined airplanes at constant altitude
• Semi-nonmatching block-interface scheme for a structured-grid-based flow solver
• Semi-nonmatching block-interface scheme for a structured-grid-based flow solver
• Simulation of viscous flow in a centrifugal compressor
• Solution of the thin-layer Navier-Stokes equations for laminar transonic flow
• Studies on numerical errors in large eddy simulation
• Studies on numerical errors in large eddy simulation
• Subsonic flutter analysis using MSC/NASTRAN
• Three-dimensional viscous/inviscid coupling in subsonic flow
• Time-accurate schemes for a multi-block Navier-Stokes solver
• TRANSF3 : a 3D grid generator based on transfinite interpolation
• Transient simulation of gas turbines including the effects of heat capacity of the solid parts
• Two-dimensional Navier-Stokes computations of subsonic and supersonic flows through turbine cascades
• Two-dimensional transonic flow calculation by interaction of Euler and boundary layer equations

inLanguage

• en
• fi

isPartOf

• Fennica

issn

• 0356-0864
• 0358-2620
• 0784-8714
• 1456-6982
• 1456-6990

name

• Hels. Univ. Technol., Lab. Aerodyn., A
• Hels. Univ. Technol., Lab. Aerodyn., B
• Helsinki University of Technology, Laboratory of Aerodynamics : Series A
• Helsinki University of Technology, Laboratory of Aerodynamics : Series B
• Helsinki University of Technology, Laboratory of Aerodynamics. Series B
• Helsinki University of Technology. Laboratory of Aerodynamics. Series A
• Helsinki University of Technology. Laboratory of Aerodynamics. Series B
• Rap. - Hels. tek. korkeak., Aerodyn. lab., B
• Rap. - Tek. korkeak., Aerodyn. lab., B
• Raportti
• Raportti / Helsingin teknillinen korkeakoulu, aerodynamiikan laboratorio. B
• Raportti / Helsingin teknillinen korkeakoulu, aerodynamiikan laboratorio. Sarja B
• Raportti / Helsingin teknillinen korkeakoulu. Aerodynamiikan laboratorio. Sarja B
• Raportti / Teknillinen korkeakoulu, aerodynamiikan laboratorio. Sarja B
• Raportti / Teknillinen korkeakoulu. Aerodynamiikan laboratorio. B
• Raportti / Teknillinen korkeakoulu. Aerodynamiikan laboratorio. Sarja B
• Rep. - Hels. Univ. Tech., Lab Aerodyn., A
• Report
• Report / Helsinki University of Technology, Faculty of Mechanical Engineering, Laboratory of Aerodynamics : Series A
• Report / Helsinki University of Technology, Laboratory of Aerodynamics : Series B
• Report / Helsinki University of Technology, Laboratory of Aerodynamics. A
• Report / Helsinki University of Technology, Laboratory of Aerodynamics. Series A
• Report / Helsinki University of Technology. Laboratory of Aerodynamics. Series A
• Report / Helsinki University of Technology. Laboratory of Aerodynamics. Series T
• Teknillinen korkeakoulu, aerodynamiikan laboratorio : Sarja A
• Teknillinen korkeakoulu, aerodynamiikan laboratorio : Sarja B
• Teknillinen korkeakoulu. Aerodynamiikan laboratorio. Raportti. Sarja B
• Teknillinen korkeakoulu. Aerodynamiikan laboratorio. Raportti. T
• Teknillinen korkeakoulu. Aerodynamiikan laboratorio. Report
• Teknillinen korkeakoulu. Aerodynamiikan laboratorio. Report. A
• Teknillinen korkeakoulu. Aerodynamiikan laboratorio. Report. Series A

P60049

• <http://rdaregistry.info/termList/RDAContentType/1020>

sameAs

• <https://issn.org/resource/issn/0356-0864>
• <https://issn.org/resource/issn/0358-2620>
• <https://issn.org/resource/issn/0784-8714>
• <https://issn.org/resource/issn/1456-6982>
• <https://issn.org/resource/issn/1456-6990>

Instances

• 1973/1987 : Teknillinen korkeakoulu
• 1973/1998 : Teknillinen korkeakoulu
• 1987-1998 : Teknillinen korkeakoulu
• 1999/2004 : Teknillinen korkeakoulu
• 1999/2007 : Teknillinen korkeakoulu