AEROTHERMOPROP

Modelica library of thermodynamic and transport properties

 Coordinatore MODELON AB 

 Organization address address: IDEON SCIENCE PARK
city: LUND
postcode: 22370

contact info
Titolo: Dr.
Nome: Jonas
Cognome: Eborn
Email: send email
Telefono: +46 46 2862203
Fax: 46462862201

 Nazionalità Coordinatore Sweden [SE]
 Totale costo 80˙000 €
 EC contributo 60˙000 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2009-02
 Funding Scheme JTI-CS
 Anno di inizio 2010
 Periodo (anno-mese-giorno) 2010-08-01   -   2011-11-30

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    MODELON AB

 Organization address address: IDEON SCIENCE PARK
city: LUND
postcode: 22370

contact info
Titolo: Dr.
Nome: Jonas
Cognome: Eborn
Email: send email
Telefono: +46 46 2862203
Fax: 46462862201

SE (LUND) coordinator 60˙000.00

Mappa


 Word cloud

Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.

pressure    celsius    entropy    deg    fluid    complete    thermodynamic    temperature    aircraft   

 Obiettivo del progetto (Objective)

'With this proposal, a Modelica library for thermodynamic properties of gases and liquids that are used as working media in aircraft, and an Excel interface to the same functions with plotting capabilities for typical thermodynamic design diagrams (Temperature-Entropy and Enthalpy-Entropy) shall be developed. It is important that the complete temperature and pressure range experienced by aircraft is covered, from -60 deg Celsius to 200 deg Celsius, depending on the fluid. The pressure range depends on the fluid, as an example a range from 150 to 1100 hPa is necessary for air. Currently available model libraries don't cover the complete range. A fixed starting date of August 1st was chosen to align the project with the original planning of the ITD activities.'

Altri progetti dello stesso programma (FP7-JTI)

CODE-TILT (2010)

Contribution to design optimization of tiltrotor components for drag reduction

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NLF-WINGHIPER (2014)

NLF Wing High Speed Performance Test

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TILTOP (2010)

Efficient Shape Optimization of Intake and Exhaust of a Tiltrotor Nacelle

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