Results 111 to 120 of about 48,655 (212)
RWF rotor-wake-fuselage code software reference guide [PDF]
The RWF (Rotor-Wake-Fuselage) code was developed from first principles to compute the aerodynamics associated with the complex flow field of helicopter configurations.
Berry, John D.
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Skyport airframe: design and manufacturing [PDF]
, 2015 Many rural areas of developing countries lack the necessary transportation infrastructure to have reliable access to basic needs. This is particularly true for medical supplies.
Clark, Thomas +3 more
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An overview of the crash dynamics failure behavior of metal and composite aircraft structures [PDF]
An overview of failure behavior results is presented from some of the crash dynamics research conducted with concepts of aircraft elements and substructure not necessarily designed or optimized for energy absorption or crash loading considerations ...
Boitnott, Richard L. +3 more
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Supersonic aircraft Patent [PDF]
, 1967 Design of supersonic aircraft with novel fixed, swept wing ...
Carlson, H. W. +4 more
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CHANCE: A FRENCH-GERMAN HELICOPTER CFD-PROJECT [PDF]
, 2006 The paper gives an overview of the CHANCE research project (partly supported by the French DPAC and DGA and the German BMWA) which was started in 1998 between the German and French Aerospace Research Centres DLR and ONERA, the University of Stuttgart and
Altmikus, Andree +4 more
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A theoretical investigation of noise reduction through the cylindrical fuselage of a twin-engine, propeller-driven aircraft [PDF]
Interior noise in the fuselage of a twin-engine, propeller-driven aircraft with two propellers rotating in opposite directions is studied analytically. The fuselage was modeled as a stiffened cylindrical shell with simply supported ends, and the effects ...
Bhat, R. B., Mixson, J. S.
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Dual towline spin-recovery device [PDF]
, 1985 A device which corrects aerodynamic spin is described wherein a parachute exerts antispin forces on an aircraft to effect spin recovery. The dual parachute towlines and are each attached to the parachute and are attached to the rear fuselage equidistant ...
White, W. L.
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Advanced emergency openings for commercial aircraft [PDF]
Explosively actuated openings in composite panels are proposed to enhance passenger survivability within commercial aircraft by providing improvements in emergency openings, fuselage venting, and fuel dump.
Bement, L. J., Schimmel, M. L.
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Automated composite ellipsoid modelling for high frequency GTD analysis [PDF]
The preliminary results of a scheme currently being developed to fit a composite ellipsoid to the fuselage of a helicopter in the vicinity of the antenna location are discussed under the assumption that the antenna is mounted on the fuselage.
Klevenow, F. T. +3 more
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Научный вестник МГТУ ГА, 2016 The present publication describes the calculation of helicopter fuselage aerodynamic characteristics and its separate elements, by computing experiment. On the basis of program commercial package CFX ANSYS the technique has been mastered and longitudinal
V. A. Ivchin +2 more
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