Aerodynamic Investigations on a Helicopter Fuselage
AIAA Applied Aerodynamics Conference [29th]
2011
Wake vortex characteristics of transport aircraft
Progress in Aerospace Sciences
2011
Vol. 47, No. 2
pp. 89-134
Pseudo-shock system structure in rectangular Laval nozzles with gaps
International Symposium on shock Waves (ISSW 28)
2011
Stemmer, C.; Adams, N.A.; Radespiel, R.; Sattelmayer, T.; Schröder, W.; Weigand, B.
Proceedings of the 2011 Summer Program within the SFBTRR40
Lehrstuhl für Aerodynamik
2011
SFB-Transgeio 40: Technologische Grundlagen für den Entwurf thermisch und mechanisch hochbelasteter Komponenten zukünftiger Raumtransportsysteme - Motivation und Struktur
Deutscher Luft- und Raumfahrtkongress
2011
SPH simulations of flow around a periodic array of cylinders confined in a channel
International Journal for Numerical Methods in Engineering
2011
86
Pages 1027–1040
Experimental Investigation of Unsteady Vehicle Aerodynamics under Time-Dependent Flow Conditions - Part 2
SAE 2011 World Congress,
April 12-14, 2011, Detroit, Michigan, USA
2011
Investigation of Unsteady Vehicle Aerodynamics under Time-Dependent Flow Conditions
Paper AIAA 2011-3349
AIAA Applied Aerodynamics Conference´[29th.],
June 27.-30., Honolulu, Hawaii, USA,
2011
Aeroacoustic Investigations of a Generic Fan-in-Wing Configuration
International Congress and Expostition on Noise Control Engineering [40th.],
Osaka Japan, September 4.-7.
2011
Numerical Investigation of Inlet distortion on a Wing-Embedded Lift Fan
Journal of propulsion and power
2011
27
1
Pages 16-28