-
1
-
-
34250849452
-
-
P. R. ASHILL, J. L. FULKER AND A. SHIRES: A Novel Technique for Controlling Shock Strength of Laminar-Flow Aerofoil Sections. In: Proceedings 1st European Forum on Laminar Flow Technology, March 16-18, 1992, Hamburg, Germany, DGLR, AAAF, RAeS, 1992, S. 175-183.
-
P. R. ASHILL, J. L. FULKER AND A. SHIRES: A Novel Technique for Controlling Shock Strength of Laminar-Flow Aerofoil Sections. In: Proceedings 1st European Forum on Laminar Flow Technology, March 16-18, 1992, Hamburg, Germany, DGLR, AAAF, RAeS, 1992, S. 175-183.
-
-
-
-
2
-
-
34250849451
-
-
G. DARGEL AND J. P. ARCHAMBAUD: Assessment of the Capability of Drag Reduction of the Shock Control Device SC Bump on Airfoil Flows and Application Aspects on Wing. In: Proceedings IUTAM Symposium on Mechanics of Passive and Active Flow Control, 7-11 September, 1998, Göttingen, Germany, G. E. A. Meier and P. R. Viswanath, Eds., Kluwer Academic Publishers, 1998, pp. 57-62,
-
G. DARGEL AND J. P. ARCHAMBAUD: Assessment of the Capability of Drag Reduction of the Shock Control Device SC Bump on Airfoil Flows and Application Aspects on Wing. In: Proceedings IUTAM Symposium on Mechanics of Passive and Active Flow Control, 7-11 September, 1998, Göttingen, Germany, G. E. A. Meier and P. R. Viswanath, Eds., Kluwer Academic Publishers, 1998, pp. 57-62,
-
-
-
-
3
-
-
0029722015
-
-
N. HANSEN UND A. OSTERMEIER: Adapting Arbitrary Normal Mutation Distributions in Evolution Strategies: The Covariance Matrix Adaption. In: Proceedings of the 1996 IEEE International Conference on Evolutionary Computation (ICEC '96), May 20-22, 1996, Nagoya, Japan, 1996, 312-317.
-
N. HANSEN UND A. OSTERMEIER: Adapting Arbitrary Normal Mutation Distributions in Evolution Strategies: The Covariance Matrix Adaption. In: Proceedings of the 1996 IEEE International Conference on Evolutionary Computation (ICEC '96), May 20-22, 1996, Nagoya, Japan, 1996, 312-317.
-
-
-
-
4
-
-
34250873155
-
-
N. KROLL, C. C. ROSSOW, D. SCHWMBORN, K. BECKER AND G. HELLER: MECAFLOW - a Numerical Flow Simulation Tool for Transport Aircraft Design. In: Proceedings of the 23rd International Congress of Aeronautical Sciences, ICAS, 2002. Toronto.
-
N. KROLL, C. C. ROSSOW, D. SCHWMBORN, K. BECKER AND G. HELLER: MECAFLOW - a Numerical Flow Simulation Tool for Transport Aircraft Design. In: Proceedings of the 23rd International Congress of Aeronautical Sciences, ICAS, 2002. Toronto.
-
-
-
-
5
-
-
8844251299
-
Flight Test of an Adaptive Configuration optimization System for Transport Aircraft
-
Tech. Rep. NASA/TM-1999-206569, NASA, Dryden Flight Research Center Edwards, California 93523-0273, Januar
-
GLENN B. GILYARD, JENNIFER GEORGIE UND JOSEPH S. BARNICKI: Flight Test of an Adaptive Configuration optimization System for Transport Aircraft. Tech. Rep. NASA/TM-1999-206569, NASA, Dryden Flight Research Center Edwards, California 93523-0273, Januar 1999.
-
(1999)
-
-
GILYARD, G.B.1
GEORGIE UND, J.2
BARNICKI, J.S.3
-
6
-
-
0038487414
-
Civil Aviation and the environmental Challange
-
J. E. GREEN: Civil Aviation and the environmental Challange. The Aeronautical Journal, Vol, 107, pp. 281-299, 2003.
-
(2003)
The Aeronautical Journal
, vol.107
, pp. 281-299
-
-
GREEN, J.E.1
-
7
-
-
85087191605
-
-
H. A. HOLDEN AND H. BABINSKY: Shock/Boundary Layer Interaction Control Usind 3D Devices. In: Aerospace Sciences Meeting and Exhibit, AIAA-2003-447, 6-9 January 2003.
-
H. A. HOLDEN AND H. BABINSKY: Shock/Boundary Layer Interaction Control Usind 3D Devices. In: Aerospace Sciences Meeting and Exhibit, AIAA-2003-447, 6-9 January 2003.
-
-
-
-
8
-
-
0028486598
-
Two-Equation Eddy-Viscosity Turbulence Models for Engineerung Applications
-
August
-
F. R. MENTER; Two-Equation Eddy-Viscosity Turbulence Models for Engineerung Applications. AIAA Journal, Vol. 32, No. 8, pp. 1598-1605, August 1994.
-
(1994)
AIAA Journal
, vol.32
, Issue.8
, pp. 1598-1605
-
-
MENTER, F.R.1
-
10
-
-
34250895962
-
-
M. KUTZBACH, TH. LUTZ AND S. WAGNER: RANS-basierte Direkte numerische Optimierung Adaptiver Flügel. Tech. Rep, DGLR-2004-055, DGLR, September 2004.
-
M. KUTZBACH, TH. LUTZ AND S. WAGNER: RANS-basierte Direkte numerische Optimierung Adaptiver Flügel. Tech. Rep, DGLR-2004-055, DGLR, September 2004.
-
-
-
-
11
-
-
84897802485
-
-
M. KUTZBACH, TH. LUTZ UND S. WAGNER; Investigations on Shock Control Bumps for Infinite Swept Wings. Paper 2004-2702, AIAA, 2004. AIAA 2nd Flow Control Conference, June 27 - July 1, 2004, Portland,OR,USA.
-
M. KUTZBACH, TH. LUTZ UND S. WAGNER; Investigations on Shock Control Bumps for Infinite Swept Wings. Paper 2004-2702, AIAA, 2004. AIAA 2nd Flow Control Conference, June 27 - July 1, 2004, Portland,OR,USA.
-
-
-
-
12
-
-
84893505912
-
Overview on drag reduction technologies for civil transport aircraft
-
Jyväskylä
-
J. RENEAUX: Overview on drag reduction technologies for civil transport aircraft. In: ECCOMAS 2004, Jyväskylä, 2004.
-
(2004)
ECCOMAS
-
-
RENEAUX, J.1
-
13
-
-
0042813564
-
Restatement of the Spalart-Allmaras Eddy-Viscosity Model in Strain-Adaptive Formulation
-
T. RUNG, U. BUNGE, M. SCHATZ AND F. THIELE: Restatement of the Spalart-Allmaras Eddy-Viscosity Model in Strain-Adaptive Formulation. AIAA Journal, Technical Notes, Vol. 41, No, 7, 2003.
-
(2003)
AIAA Journal, Technical Notes
, vol.41
, Issue.7
-
-
RUNG, T.1
BUNGE, U.2
SCHATZ, M.3
THIELE, F.4
-
14
-
-
33751241786
-
EUROSHOCK - Drag Reduction by passive Shock Control, AERS-CT92-0049
-
of, Vieweg Verlag
-
E. STANEWSKY, J. FULKER, J. DELERY AND J. GEISSLER: EUROSHOCK - Drag Reduction by passive Shock Control, AERS-CT92-0049. Vol. 56 of Notes on Numerical Fluid Mechanics, Vieweg Verlag, 1997.
-
(1997)
Notes on Numerical Fluid Mechanics
, vol.56
-
-
STANEWSKY, E.1
FULKER, J.2
DELERY, J.3
GEISSLER, J.4
-
15
-
-
0035472772
-
Adaptive wing and flow control technology
-
E. STANEWSKY: Adaptive wing and flow control technology. Progress in Aerospace Sciences, Vol. 37, pp. 583-667, 2001.
-
(2001)
Progress in Aerospace Sciences
, vol.37
, pp. 583-667
-
-
STANEWSKY, E.1
-
17
-
-
84893357372
-
Design of Adaptive Transonic Airfoils by Means of Numerical Optimisation
-
11-14 September, Barcelona, Spain
-
ANDREAS SOMMERER, THORSTEN LUTZ AND SIEGFRIED WAGNER: Design of Adaptive Transonic Airfoils by Means of Numerical Optimisation. In: Proceedings of ECCOMAS 2000, European Congress on Computational Methods in Applied Sciences and Engineering, 11-14 September, 2000, Barcelona, Spain, 2000.
-
(2000)
Proceedings of ECCOMAS 2000, European Congress on Computational Methods in Applied Sciences and Engineering
-
-
SOMMERER, A.1
LUTZ, T.2
WAGNER, S.3
-
18
-
-
84871878807
-
Numerical Optimisation of Adaptive Transonic Airfoils with Variable Camber
-
27 August, 1 September, Harrogate, UK
-
ANDREAS SOMMERER, THORSTEN LUTZ AND SIEGFRIED WAGNER: Numerical Optimisation of Adaptive Transonic Airfoils with Variable Camber. In: Proceedings of the 22nd International Congress of the Aeronautical Sciences, 27 August - 1 September, 2000, Harrogate, UK, 2000.
-
(2000)
Proceedings of the 22nd International Congress of the Aeronautical Sciences
-
-
SOMMERER, A.1
LUTZ, T.2
WAGNER, S.3
-
20
-
-
77955528145
-
Structural Concepts and Aerodynamic Design of Shock Control Bumps
-
Toronto, Canada
-
WOLF WADEHN, ANDREAS SOMMERER, THORSTEN LUTZ, DMITRI FOKIN, GÜNTER PRITSCHOW AND SIEGFRIED WAGNER: Structural Concepts and Aerodynamic Design of Shock Control Bumps. In: Proceedings of the 23rd International Congress of the Aeronautical Sciences, September 8 - 13, 2002, Toronto, Canada, 2002.
-
(2002)
Proceedings of the 23rd International Congress of the Aeronautical Sciences, September 8
, vol.13
-
-
WADEHN, W.1
SOMMERER, A.2
LUTZ, T.3
FOKIN, D.4
PRITSCHOW, G.5
WAGNER, S.6
|