Helicopter route chart, New York.

Aeronautical chart showing designated helicopter routes and control areas.

Tidal current charts, New York Harbor.

First ed. issued as its Special publication, no. 152.

Map of the bays, harbors, and rivers around New York : showing the channels, soundings, lighthouses, buoys &c., and the complete topography of the surrounding country : including Hempstead, Sandy-Hook, South-Amboy, Newark, Yonkers, N. Rochelle & Glen Cove /

Relief shown by hachures. Depths shown by contours and soundings.

New a posteriori error estimator and adaptive mesh refinement strategy for 2-D crack problems

A posteriori error estimation and adaptive refinement technique for fracture analysis of 2-D/3-D crack problems is the state-of-the-art. The objective of the present paper is to propose a new a posteriori error estimator based on strain energy release rate (SERR) or stress intensity factor (SIF) at the crack tip region and to use this along with the stress based error estimator available in the literature for the region away from the crack tip. The proposed a posteriori error estimator is called the K-S error estimator. Further, an adaptive mesh refinement (h-) strategy which can be used with K-S error estimator has been proposed for fracture analysis of 2-D crack problems. The performance of the proposed a posteriori error estimator and the h-adaptive refinement strategy have been demonstrated by employing the 4-noded, 8-noded and 9-noded plane stress finite elements. The proposed error estimator together with the h-adaptive refinement strategy will facilitate automation of fracture analysis process to provide reliable solutions.

New Look at Kirchhoff's Theory of Plates

KIRCHHOFF’S theory [1] and the first-order shear deformation theory (FSDT) [2] of plates in bending are simple theories and continuously used to obtain design information. Within the classical small deformation theory of elasticity, the problem consists of determining three displacements, u, v, and w, that satisfy three equilibrium equations in the interior of the plate and three specified surface conditions. FSDT is a sixth-order theory with a provision to satisfy three edge conditions and maintains, unlike in Kirchhoff’s theory, independent linear thicknesswise distribution of tangential displacement even if the lateral deflection, w, is zero along a supported edge. However, each of the in-plane distributions of the transverse shear stresses that are of a lower order is expressed as a sum of higher-order displacement terms. Kirchhoff’s assumption of zero transverse shear strains is, however, not a limitation of the theory as a first approximation to the exact 3-D solution.

New method of calculating calorific values from elemental compositions of fossil fuels

A new method of calculating the calorific values of fossil fuels from their chemical composition has been developed, based on the concept that heats of reaction of stoichiometric fuel-oxidizer systems are rectilinearly related with the total oxidizing or reducing valancies of the mixture. The calorific value of fossil fuels has been shown to be directly related to the net reducing valencies of the fuel. The proposed method is simple and compares favourably with the other prominent methods reported in the literature.

New rational interpolation functions for finite element analysis of rotating beams

A rotating beam finite element in which the interpolating shape functions are obtained by satisfying the governing static homogenous differential equation of Euler–Bernoulli rotating beams is developed in this work. The shape functions turn out to be rational functions which also depend on rotation speed and element position along the beam and account for the centrifugal stiffening effect. These rational functions yield the Hermite cubic when rotation speed becomes zero. The new element is applied for static and dynamic analysis of rotating beams. In the static case, a cantilever beam having a tip load is considered, with a radially varying axial force. It is found that this new element gives a very good approximation of the tip deflection to the analytical series solution value, as compared to the classical finite element given by the Hermite cubic shape functions. In the dynamic analysis, the new element is applied for uniform, and tapered rotating beams with cantilever and hinged boundary conditions to determine the natural frequencies, and the results compare very well with the published results given in the literature.

New Energetic Epoxy Binders

A new class of epoxy resins having N-N bonds in the backbone has been synthesized with a view to explore their properties as energetic binders. The N-epoxidation of bis-dicarbonylhydrazones of adipic, azelaic and sebacic dihydrazides results in the formation of viscous resins having epoxide end groups. The resins have been characterized by the elemental and end group analyses, IR and NMR spectra. Relevant properties for their use as binders in solid propellants, such as thermal stability, heat of combustion, burn rate and performance parameters of AP-based propellant systems, have been evaluated. A significant increase in the burn rate of AP-based propellants noticed, is perhaps related to the exothermicity of the binder decomposition and the reactivity of N-N bonds with perchloric acid formed during the combustion of AP.

From New Inlet to Absecon Inlet.

Scale 1:80,000.

South Carolina aeronautical chart

This document is a fold-out aeronautical chart with diagrams of South Carolina airports.

Aeronautical Information Geoservices

Aeronautical charts underlie the representation of aeronautic geographic information that supports pilots in flight. Nevertheless, charts become complex due to the high density of data and the different kinds that support each phase of flight. These features make difficult using them on board. After conducting a study that aims to understand and to evaluate pilot’s needs related to Geographic Information, it is proposed a solution to implement a platform based on geographic information standards (OGC, ISO) and supported by a distributed Web architecture. This platform facilitates the use, retrieval, updating of information and its exchange among different institutions through private and public users. As a first element to ensure interoperability and the harmonisation of information, we propose an aeronautical metadata profile that sets guidelines and elements for its description. This profile meets the standards set by ICAO, Eurocontrol and ISO. The platform offers three levels of access to data through different types of devices and user profiles. This paper suggests an alternative and reliable way for distributing aeronautical geoinformation, focusing on specific functions or displaying and querying.

Geoservices for Aeronautical Navigation

Aeronautical charts underlie the representation of aeronautic geographic information that supports pilots in flight. Nevertheless, the charts become complex due to the high density of data and the different kinds of charts that support each phase of flight. These features make difficult using them on board. After conducting a study, with civil Spaniard pilots, that aims to understand and to evaluate their needs related to Geographic Information, it is proposed a solution to implement a platform based on geographic information standards (OGC, ISO) and supported by a distributed Web architecture. This platform facilitates the use, retrieval, updating of information and its exchange among different institutions through private and public users. As a first element to ensure interoperability of information, we suggest an aeronautical metadata profile that sets guidelines and elements for its description. The metadata profile meets the standards set by ICAO, Eurocontrol and ISO. The platform offers three levels of access to data through different types of devices and user profiles. Thus, aeronautical institutions could edit data while pilot is on board accessing digital aeronautical charts through a laptop or Table PC. This paper suggests an alternative and reliable way for distributing aeronautical geoinformation, focusing on specific functions or displaying and querying.

Summary of National Ocean Survey technical publications and charts /

Cover title.

Claves para la requerida universalización simbológica de las Cartas Aeronáuticas

The aeronautical charts are a convenient means to provide aeronautical information in a manageable, condensed, and coordinated way. Despite having an extensive regulatory legislation backed by the International Civil Aviation Organization (ICAO), this kind of specialized mapping is defined by a marked symbolical disparity between the different editions published by countries and publishers. This implies not to follow the uniformity and consistency principles that ICAO have identified as essential to help ensure the safety of international civil aviation. Plans for the implementation of a global interoperability of aeronautical information require urgently rethink the way in which, so far, this information has been published and disseminated. A single, transverse, and independent symbolical specification would contribute to the generation of a well defined final-product that provides general purpose aeronautical information for an unequivocal interpretation. The contribution of this article is the verification of the real possibilities for the definition of a general specification that provides the mechanisms for a reliable, indisputable, and legible reading of aeronautical charts under any operational circumstances and conditions. Such conditions must be aligned with the specificities of any country, publishers or crew.

Diseño de la metodología para el control de la calidad de la exactitud posicional de la serie L del Centro geográfico del Ejército de Tierra (CEGET).

En este trabajo se ha evaluado la hoja correspondiente a la 1074 del Mapa Topográfico Nacional (Tahivilla) o 13-47 de la “serie L” (1:50.000) según la denominación del Centro Geográfico del Ejército de Tierra en tres formatos distintos; formato en impreso en papel, formato raster, y formato vectorial. Con este Proyecto Fin de Carrera se pretende desarrollar una metodología adecuada para el control de calidad en la exactitud posicional de la serie L del Centro Geográfico del Ejército de Tierra (C.E.G.E.T.), así como aplicar, ampliar y afianzar los conocimientos adquiridos a lo largo de los cursos de la titulación de Ingeniero Técnico en Topografía. Se debe mencionar la necesidad de realizar este tipo de controles a la cartografía editada en los distintos formatos, ya que se pueden obtener enseñanzas que afecten al flujo de producción, además de cumplir los estándares marcados por la alianza para los centros productores de cartografía de los países miembros de la OTAN. Según el estudio expuesto en este proyecto, se puede afirmar que el control de calidad de la exactitud posicional según lo recogido en el STANAG 2215, “Evaluation of land maps, aeronautical charts and digital topographic data”, la clasificación OTAN para dicha serie, es AA-M10. La hoja de “Tahivilla” se eligió por se una de las últimas editadas por el CEGET, y por responder a unas características generales representaticas de la serie L. El Proyecto Fin de Carrera, está dirigido a todos los expertos en la materia, personal docente y alumnos de Ingeniería Técnica en Topografía y alumnos de Grado en Ingeniería Geomática y Topografía. Este proyecto se realiza como parte del control de calidad que el CEGET realiza a la serie L. En concreto de la última edición publicada en el año 2010. Además, la Escuela Técnica Superior de Ingenieros en Topografía Geodesia y Cartografía mediante el convenio firmado con el CEGET, se compromete a colaborar activamente con dicho Centro en las necesidades que cada Proyecto Fin de Carrera surja de este convenio.