Influence of wing elasticity on dynamic derivatives of transport aircraft

48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2010, Pages

  Loeser, Thomas ^a   Hübner, Andreas René ^b  

^a DNW NWB   (Germany)

^b GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT CONFIGURATIONS; DYNAMIC DERIVATIVES; DYNAMIC TESTS; HIGH SPEED VIDEO CAMERAS; LOW-SPEED WIND TUNNEL; ON DYNAMICS; STATIC AND DYNAMIC; WING DEFORMATION;

AEROSPACE ENGINEERING; BENDING (DEFORMATION); ELASTICITY; FLIGHT DYNAMICS; PRESSURE EFFECTS; TESTING; VIDEO CAMERAS;

TRANSPORT AIRCRAFT;

EID: 78649883376     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

1. Kausche, G., Otto, H., Siebert, R. and Christ, D., "The Low-Speed Wind Tunnel at DFVLR in Brunswick (Status 1988)", DFVLR-Mitt. 88-25 (1988).
2. Loeser, T., Bergmann, A., "Development of the Dynamic Wind Tunnel Testing Capabilities at DNW-NWB". AIAA-2003-453.
3. Bergmann, A. et al. "Experimental and Numerical Research on the Aerodynamics of Unsteady Moving Aercraft". In: Progress in Aerospace Sciences, Elsevier, Vol. 44 (2008).
4. Bergmann, A. et al. "MPM". USA Patent Application. Pub. No. US 2006/0254380 A1. Nov. 2006.
5. Hübner, A., "Experimental and Numerical Investigations of Unsteady Aerodynamic Derivatives for Transport Aircraft Configurations". AIAA-2007-1076.
6. Hübner, A., Bergmann, A., Loeser, T., "Experimental and Numerical Investigations of Unsteady Force and Pressure Distributions of Moving Transport Aircraft Configurations". AIAA-2009-91.
7. Kirmse, T., "Model Deformation Measurements in DNW-NWB within the DLR Project ForMEx". Conference Proceedings, CD-ROM (S12-1), ODAS 2007. 8th ONERA-DLR Aerospace Symposium, Göttingen, Oct. 17th -19th 2007.
8. Nyland, T.W., Englund, D.R., Anderson, R.C., "On The Dynamics of short Pressure Probes: Some Design Factors Affecting Frequency Response". NASA TN D-6151 (1971).
9. Müller, R.H.G., "picCOLOR - Wissenschaftliche und Industrielle Bildverarbeitung und Bildanalyse. Dokumentation für die Programmversion V3.3". Forschungsinstitut für Bildverarbeitung, Umwelttechnik und Strömungsmechanik, Düsseldorf, (2000).
10. Kilian, T., "Einfluss der Flügeldeformation der DLR-F12 Konfiguration bei der experimentellen und numerischen Ermittlung der statischen und dynamischen Derivative". Diploma Thesis No. 02/2008. DLR Institute of Aerodynamics and Flow Technology, (March 2009).
11. Loeser, T., "Experimental Research of Dynamic Derivatives of Unsteady Moved Aircraft". In "Experimental determination of dynamic stability parameters", VKI LS 2008-02, The von Karman Institute for Fluid Dynamics, Rhode-St-Genèse, Belgium.
12. Hummel, D, Loeser, T., "Low Speed Wind Tunnel Experiments on a Delta Wing Oscillating in Pitch". ICAS 98-393 (1998).
13. Fritz, W., "Unsteady Navier-Stokes Calculations for a Delta Wing Oscillating in Pitch". ICAS 98-241 (1998).