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Flugzeug
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Experimental analysis of the flow over an owl-based wing geometry
Time-variant aerodynamics for torsional motion of large-turning airfoils
Some theoretical considerations of a stall proof airplane
Effects of a spin chute installation on spin characteristics
The Wright Brothers: First aeronautical engineers and test pilots
Planar velocimetry of jet/fin interaction on a full-scale flight vehicle configuration
Toward integrated structural design with advanced composites
Helicopter vibration reduction using fixed-system auxiliary moments
Optimal control-surface locations for flexible aircraft
Flutter simulations of a T-tail configuration using non-linear aerodynamics
Aerodynamic development of a high pressure leading edge blowing boundary layer control system
Smart fins: Analytical modeling and basic design concepts
Advanced techniques for clearance of flight control laws
Some practical aspects of viscous drag reduction concepts
Design, manufacture and test of a composite material rocket fin
Tail buffet alleviation of high-performance twin-tail aircraft using piezostack actuators
An examination of blunt-fin induced shock wave turbulent boundary layer interactions
Speed stability: The difference between rotors and wings
Numerical simulation of high-incidence flow over the F-18 fuselage forebody
The Boeing 747-400 upper rudder control system with triple tandem valve
Fuselage structural-acoustic modeling for structure-borne interior noise transmission
Wing-tail interaction flutter revisited
Germany's upgrade plans: Keeping Eurocopter busy
Developments in adhesively bonding the wings of the SAAB 340 and 2000 aircraft
Study of junction and tip vortices using particle displacement velocimetry
The characterization of non-stationary buffet environments
Enhanced structural damage tolerance of CFRP primary structures by Z-pin reinforcement
The all-composite aircraft. Fact or fiction?
Nonlinear vibrations of periodically stiffened plates
Airbrake induced fin buffet loads on fighter aircraft
Computational analysis of drag reduction techniques for afterbody/nozzle/empennage configurations