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Airship Technology
4.0
1 votes
Structural dynamic model obtained from flight use with piloted simulation and handling qualities analysis
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Design trends for Army/Air Force airplanes in the United States
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Developing a workstation-based, real-time simulation for rapid handling qualities evaluations during design
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The use of the Regier number in the structural design with flutter constraints
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Design of fuselage shapes for natural laminar flow
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A design procedure for the handling qualities optimization of the X-29A aircraft
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Aerodynamic shape optimization directed toward a supersonic transport using sensitivity analysis
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Supersonic civil airplane study and design
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Development of stitched/RTM primary structures for transport aircraft
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Descriptions of Cranfield aircraft group design projects (1979-96)
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Optimum aerodynamic design via boundary control
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Multi-lab comparison of R-curve methodologies
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Development of direct-inverse 3-D method for applied aerodynamic design and analysis
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Fuselage design for a specified Mach-sliced area distribution
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Aeroelasticity of wing and wing-body configurations on parallel computers
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The lift-fan aircraft
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Second NASA Advanced Composites Technology Conference
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System synthesis in preliminary aircraft design using statistical methods
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Demonstration of a probilistic technique for the determination of economic viability of very large transport configurations
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Screech tones from rectangular jets with spanwise oblique shock-cell structures
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Direct adaptive aircraft control using dynamic cell structure neural networks
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Case study in aircraft design
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Manual on the flight of flexible aircraft in turbulence
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