Mission - adaptive wing camber control systems for transport aircraft

3rd Applied Aerodynamics Conference, 1985

Volumn , Issue , 1985, Pages

  Renken, Jürgen H ^a  

^a AIRBUS GROUP INNOVATIONS   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT CONTROL; CAMBERS; FLIGHT CONTROL SYSTEMS; TRANSPORT AIRCRAFT;

AUTOMATIC FLIGHT; CAMBER CONTROL; MECHANICAL VERIFICATION; MISSION ADAPTIVE WINGS; RESEARCH PROGRAMS; VARIABLE CAMBERS; WING PROFILES;

ADAPTIVE CONTROL SYSTEMS;

EID: 84915226631     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

1. SIEWERT, R.F., Naval Air Systems Command Washington, DC, USA and WHITEHEAD, R.E., Office of Naval Research, Arlington, VA, USA: ‘Analysis of advanced variable camber concepts’
2. ‘Hybrid laminar flow control study; final technical report’ Boeing commercial airplane company/NASA CR 165930, 1982.
3. HILBIG, R., WAGNER, H., MBB-UT ‘Variable wing camber for civil transport aircraft’. ICAS-Paper 85-5-2-1 Toulouse 1984.
4. SZODRUCH, J., MBB-UT, ‘The influence of camber variation on the aerodynamics of civil transport aircraft’. AIAA-Paper 85-0353, Reno, Nov. 1985.
5. SOBIECZKY, H., DFVLR ‘Computational methods for the design of adaptive airfoils and wings’, published in; Proceedings of the Third GAHM- conference on Numerical Methods in Fluid. Mechanics, DFVLR, COLOGNE, Oct. 1979, Ed. E.H. HIRSCHEL.
6. VOOGT, N., SLOOFF, J.W., ‘Advanced aerodymanic wing design for commercial transports - Review of a technology program in the Netherlands’. ICAS-82-5.6.1, SEATTLE 1982.
7. LAMBREGTS, A. A., ‘Functional integration of vertical flight path and speed control using energy principles’, Boeing Commercial Company, Seattle, NASA-Conference Publication 2296.