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Flugzeugbau
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Description and test results of a water basin to determine ground effect in hover using small models
Stretch forming matches fabricating "wits" with a mini-giant
Controlled flow structural adhesives for film reticulation
Propulsive-lift noise of an upper surface blown flap configuration
Fabrication methods for YF-12 wing panels for the supersonic cruise aircraft research program
Bonding development of improved adhesives for acoustic structures
Lifetime variability characterization of adhesively bonded composite-to-metal joints
Effects of interactive graphics on the aircraft design process
Strukturauslegung unter Beruecksichtigung der Schwingfestigkeit im Leichtbau
Engine/Airframe Compatibility Studies for Supersonic Cruise Aircraft
Extended energy management methods for flight performance optimization
Physicochemical testing ofaltered compositio n3501-6 epoxy resin
B-52 control configured vehicles maneuver load control system analysis and flight test results
Supersonic jet noise suppression with multitube nozzle/ejectors
Anwendung des Diffusionsschweissens - Diffusionsschweissen grosser Bauteile aus TiAl6V4
An experimental investigation of the drag on a circular cylinder and curved shell in transonic flow
Fiberglass reinforced plastic BI-PAC vibration and rough handling tests
Effect of forward speed on jet wing/flap interaction noise
Spannungsintensitaetsfaktoren von ebenen, versteiften Blechstrukturen
Design, fabrication and test of an F-14 composite overwing fairing
Potential flow about three-dimensional lifting configurations with application to wings and rotors
Deburring: Some of the problems and requirements of the aircraft industry
Off they go (advanced composites, that is) into the wild blue yonder
A reliability-based cost effective fail-safe design procedure
Influence of subsurface defects on fatigue properties of titanium alloys
Developing methods for tracking crack growth damage in aircraft
Swirling-flow jet noise suppressors for aircraft engines
An improved mach-box approach for the calculation of supersonic oscillatory pressure distribution
Optimization of continuous one-dimensional structures under steady harmonic excitation
A new role for structures technology in aircraft configuration development
Optimal periodic proof test based on cost-effective and reliability criteria
Design, facbrication and test of an F-14 composite overwing fairing