NLF-WINGHIPER

NLF Wing High Speed Performance Test

 Coordinatore EUROPEAN TRANSONIC WINDTUNNEL GMBH 

 Organization address address: Ernst Mach Strasse
city: KOELN
postcode: 51147

contact info
Titolo: Dr.
Nome: Peter
Cognome: Guntermann
Email: send email
Telefono: +49 2203 609113
Fax: +49 2203 609 124

 Nazionalità Coordinatore Germany [DE]
 Totale costo 1˙499˙384 €
 EC contributo 1˙124˙538 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2013-03
 Funding Scheme JTI-CS
 Anno di inizio 2014
 Periodo (anno-mese-giorno) 2014-07-01   -   2015-03-31

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    EUROPEAN TRANSONIC WINDTUNNEL GMBH

 Organization address address: Ernst Mach Strasse
city: KOELN
postcode: 51147

contact info
Titolo: Dr.
Nome: Peter
Cognome: Guntermann
Email: send email
Telefono: +49 2203 609113
Fax: +49 2203 609 124

DE (KOELN) coordinator 1˙124˙538.00

Mappa


 Word cloud

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

investigations    flow    quality    turbulent    laminar    model    wing    drag    tool   

 Obiettivo del progetto (Objective)

'The primary innovative approach and the major aim of the investigations being covered here is in the first instance to perform reliable and high quality procedures for laminar wing testing under and near flight conditions at high Reynolds numbers in ETW. Beside confirming a number of already mature and successfully applied measuring techniques, these investigations will allow to validate a new evaluation process by quantitatively determining areas of turbulent flow on the wing, e.g. generated by turbulent wedges inside the laminar flow region.. Calculating the difference in drag due to laminar and turbulent flow by post-processing forms a tool for correcting the overall drag as measured by the balance.

A second subject of interest is the surface quality of the model to be tested. Special attention will be given to the cleanliness of the model on preparation and the eventual contamination while testing.

The experiments will improve the understanding of the flow and the performance of airplanes and are an indispensable tool for airframe manufacturers. At the end the project will help to safe resources like fuel, to reduce the pollution of environment by exhaust gases and noise and finally to increase the safety of flights.'

Altri progetti dello stesso programma (FP7-JTI)

PURE (2013)

Development of Auxiliary Power Unit for Recreational yachts

Read More  

ELECFILTER (2012)

DESIGN OF COMPRESSOR AIR INLET PROTECTION FOR ELECTRICAL ECS

Read More  

FUSES 2014 (2014)

CURRENT LIMITING DEVICE TO ADDRESS DC AERONAUTICS POWER DISTRIBUTION SYSTEMS

Read More