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11 resultados encontrados.

Tipos de recurso: Libro electrónico Artículo Revista Tesis Capítulo
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Design and Realization of an Unmanned Aerial Rotorcraft Vehicle Using Pressurized Inflatable Structure
Artículo
Material complementario disponible Artículo DOAJ
Nirmal Sadasivan · Embry-Riddle Aeronautical University · 2019 · ISSN 2374-6793
Unmanned aerial rotorcraft vehicles have many military, commercial and civil applications. There is a necessity to advance the performance on several ranges of rotorcraft for using these vehicles successfully in the expa...
LCC LCC:Motor vehicles. Aeronautics. AstronauticsIdioma eng
Material complementario disponibleEl enlace apunta a material asociado, anexos, tablas, datos o página complementaria. No se marca como libro/texto completo.
Material complementario
Optimization and Analysis of an Elite Electric Propulsion System
Artículo
Acceso abierto Artículo DOAJ
Mehakveer Singh et al · Embry-Riddle Aeronautical University · 2019 · ISSN 2374-6793
Abstract- Electric propulsion has a promising system to create new possibilities in this technological era as well as control the harmful gaseous emission. This paper put a vision on several parameters of electric propul...
LCC LCC:Motor vehicles. Aeronautics. AstronauticsIdioma eng
Acceso abiertoRuta libre sin proxy. Acceso recomendado cuando no hay suscripción activa.
Open Access
A thrust equation treats propellers and rotors as aerodynamic cycles and calculates their thrust without resorting to the blade element method
Artículo
Acceso abierto Artículo DOAJ
Phillip - Burgers · Embry-Riddle Aeronautical University · 2019 · ISSN 2374-6793
The lift generated by a translating wing of known translational speed, lift coefficient and area is calculated by a simple equation. A propeller or rotor generating thrust share the same aerodynamic principles but their ...
LCC LCC:Motor vehicles. Aeronautics. AstronauticsIdioma eng
Acceso abiertoRuta libre sin proxy. Acceso recomendado cuando no hay suscripción activa.
Open Access
Aerodynamic Design and Exploration of a Blended Wing Body Aircraft at Subsonic Speed
Artículo
Acceso abierto Artículo DOAJ
Sam Dakka et al · Embry-Riddle Aeronautical University · 2019 · ISSN 2374-6793
Blended Wing Body (BWB) is a novel aircraft concept which provides many different aerodynamic benefits over conventional aircrafts design. This research investigated the BWB design, L/D characteristics, surface pressure ...
LCC LCC:Motor vehicles. Aeronautics. AstronauticsIdioma eng
Acceso abiertoRuta libre sin proxy. Acceso recomendado cuando no hay suscripción activa.
Open Access
Comparison of Fixed-Wing Unmanned Aircraft Systems (UAS) for Agriculture Monitoring
Artículo
Acceso abierto Artículo DOAJ
Joseph Cerreta et al · Embry-Riddle Aeronautical University · 2019 · ISSN 2374-6793
Florida citrus growers need inexpensive methods to observe citrus plants to detect disease and stress consistently. Health vegetation indices, such as the Normalized Difference Vegetation Index (NDVI) collected from Unma...
LCC LCC:Motor vehicles. Aeronautics. AstronauticsIdioma eng
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Open Access
Design Guidelines for Supersonic Aircrafts in Civil Aviation
Artículo
Acceso abierto Artículo DOAJ
Tridib Banerjee · Embry-Riddle Aeronautical University · 2019 · ISSN 2374-6793
There exists no publication currently available to the scholars that address in detail, every aspect of designing a modern supersonic aircraft for civil aviation. This paper aims to resolve that issue. It reviews all the...
LCC LCC:Motor vehicles. Aeronautics. AstronauticsIdioma eng
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Open Access
Effect of chemical reactions on the fluidic thrust vectoring of an axisymmetric nozzle
Artículo
Acceso abierto Artículo DOAJ
Rachid CHOUICHA et al · Embry-Riddle Aeronautical University · 2019 · ISSN 2374-6793
Abstract: During the last years, several thrust control systems of aerospace rocket engines have been developed. The fluidic thrust vectoring is one of them; it is simple in design and offers a substantial gain in weigh...
LCC LCC:Motor vehicles. Aeronautics. AstronauticsIdioma eng
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Open Access
FE Modeling Methodology for Load Analysis and Preliminary Sizing of Aircraft Wing Structure
Artículo
Acceso abierto Artículo DOAJ
Jun Hwan Jang et al · Embry-Riddle Aeronautical University · 2019 · ISSN 2374-6793
It is a critical part at the basic design phase of aircraft structural design to build a finite element model and it will have a direct impact on time and cost for airframe structure development. In addition, the objecti...
LCC LCC:Motor vehicles. Aeronautics. AstronauticsIdioma eng
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Open Access
In-flight Wingtip Folding: Inspiration from the XB-70 Valkyrie
Artículo
Acceso abierto Artículo DOAJ
Gaétan X Dussart et al · Embry-Riddle Aeronautical University · 2019 · ISSN 2374-6793
Wingip folding can be used to extend aircraft wingspan, allowing designers to take advantage of reduced induced drag whilst respecting ground operational limitations. Such devices can also be used in-flight for a variety...
LCC LCC:Motor vehicles. Aeronautics. AstronauticsIdioma eng
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Open Access
Satellite Maintenance: An Opportunity to Minimize the Kessler Effect
Artículo
Acceso abierto Artículo DOAJ
Bettina M Mrusek · Embry-Riddle Aeronautical University · 2019 · ISSN 2374-6793
Recently, there has been an emphasis on the growing problem of orbital debris. While the advantages of placing satellites into space are numerous, advances in satellite technology combined with the growth of the industry...
LCC LCC:Motor vehicles. Aeronautics. AstronauticsIdioma eng
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Open Access
Integrated Design of D.D.I., Filament Winding and Curing Processes for Manufacturing the High Pressure Vessel (Type II)
Artículo
Acceso abierto Artículo DOAJ
Hyoseo Kwak et al · KeAi Communications Co., Ltd · 2019 · ISSN 1000-9345
Abstract As energy crisis and environment pollution all around the world threaten the widespread use of fossil fuels, compressed natural gas (CNG) vehicles are explored as an alternative to the conventional gasoline powe...
LCC LCC:Ocean engineering; TENDOk1lY2hhbmljYWwgZW5naW5lZXJpbmcgYW5kIG1hY2hpbmVyeQ~~Idioma eng
Acceso abiertoRuta libre sin proxy. Acceso recomendado cuando no hay suscripción activa.
Open Access