Versenden
Drucken
Schmitt, V. und Archambaud, J.P. und Horstmann, K.H. und Quast, A. (2001) Hybrid Laminar Fin Investigations. In: RTO AVT Symposium on Active Control Technology for Enhanced Performance Operational Capabilities of Military Aircraft, Land Vehicles and Sea Vehicles, 1-1-1-10. RTO AVT Symposium on Active Control Technology for Enhanced Performance Operational Capabilities of Military Aircraft, Land Vehicles and Sea Vehicles, Braunschweig (de), 08.-11.05.2000.
Dieses Archiv kann nicht den Volltext zur Verfügung stellen.
Kurzfassung
The paper deals with the aerodynamic design of laminar flow wings. The main design concepts at present applied which are Natural Laminar Flow (NLF) based on favorable pressure gradients and Hybrid Laminar Flow (HLF) using in addition leading edge suction are presented and discussed. The essential role of a reliable transition prediction in the design process is pointed out. Specific design features of the suction system are also addressed. In addition, some aspects of the off-design problems are raised.
| elib-URL des Eintrags: | https://elib.dlr.de/12370/ | ||||||||||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Dokumentart: | Konferenzbeitrag (Paper) | ||||||||||||||||||||
| Zusätzliche Informationen: | LIDO-Berichtsjahr=2002, | ||||||||||||||||||||
| Titel: | Hybrid Laminar Fin Investigations | ||||||||||||||||||||
| Autoren: |
| ||||||||||||||||||||
| Datum: | 2001 | ||||||||||||||||||||
| Erschienen in: | RTO AVT Symposium on Active Control Technology for Enhanced Performance Operational Capabilities of Military Aircraft, Land Vehicles and Sea Vehicles | ||||||||||||||||||||
| Open Access: | Nein | ||||||||||||||||||||
| Gold Open Access: | Nein | ||||||||||||||||||||
| In SCOPUS: | Nein | ||||||||||||||||||||
| In ISI Web of Science: | Nein | ||||||||||||||||||||
| Seitenbereich: | 1-1-1-10 | ||||||||||||||||||||
| Name der Reihe: | RTO MP-051 | ||||||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||||||
| Stichwörter: | Aerodynamic design, laminar flow wing, natural laminar flow, hybrid laminar flow, transition prediction, windtunnel tests, flight tests | ||||||||||||||||||||
| Veranstaltungstitel: | RTO AVT Symposium on Active Control Technology for Enhanced Performance Operational Capabilities of Military Aircraft, Land Vehicles and Sea Vehicles, Braunschweig (de), 08.-11.05.2000 | ||||||||||||||||||||
| HGF - Forschungsbereich: | Verkehr und Weltraum (alt) | ||||||||||||||||||||
| HGF - Programm: | Luftfahrt | ||||||||||||||||||||
| HGF - Programmthema: | keine Zuordnung | ||||||||||||||||||||
| DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||
| DLR - Forschungsgebiet: | L ST - Starrflüglertechnologien | ||||||||||||||||||||
| DLR - Teilgebiet (Projekt, Vorhaben): | L - Konzepte & Integration (alt) | ||||||||||||||||||||
| Standort: | Köln-Porz , Braunschweig , Göttingen | ||||||||||||||||||||
| Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik | ||||||||||||||||||||
| Hinterlegt von: | Grant, Claudia | ||||||||||||||||||||
| Hinterlegt am: | 31 Jan 2006 | ||||||||||||||||||||
| Letzte Änderung: | 14 Jan 2010 18:53 |
Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags
