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Aircraft Design Rds Student

Author: Daniel P. Raymer
Publisher: Amer Inst of Aeronautics &
ISBN: 9781600869211
Size: 64.56 MB
Format: PDF
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This textbook presents the process of aircraft conceptual design as seen in industry aircraft design groups. It contains design methods, illustrations, tips, explanations and equations, and has extensive appendices with key data for design.

Aircraft Design

Author: Daniel P. Raymer
Publisher: Amer Inst of Aeronautics &
ISBN: 9781563472817
Size: 61.99 MB
Format: PDF, Docs
View: 3477
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This textbook presents the process of aircraft conceptual design as seen in industry aircraft design groups. It contains design methods, illustrations, tips, explanations and equations, and has extensive appendices with key data for design.

Flugzeugtriebwerke

Author: Willy J.G. Bräunling
Publisher: Springer-Verlag
ISBN: 3642345395
Size: 27.37 MB
Format: PDF, ePub, Mobi
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Dieses Buch bietet eine umfassende und detaillierte Behandlung der wichtigsten Fragen zu Flugzeug- und Gasturbinenantrieben für Ingenieure, ein hervorragendes Kompendium für fortgeschrittene Studenten. Es hat sich in kurzer Zeit einen herausragenden Platz in der Fachliteratur erobert. Eine leicht verständliche Einführung in die zugehörigen Aspekte der Aerodynamik und der Thermodynamik vereinfacht den Einstieg in die Theorie ganz erheblich und schafft so sichere Grundlagen. In weiteren Abschnitten werden entscheidende Begriffe und technisch/physikalische Zusammenhänge anschaulich definiert und parametrische Kreisprozessanalysen idealer und realer Triebwerke vorgestellt. Eine Klassifizierung der Flugzeugtriebwerke und Funktionsbeschreibungen der Hauptkomponenten fehlen ebenso wenig wie die Thermo- und Aerodynamik thermischer Turbomaschinen. Anhand zahlreicher durchgerechneter Beispiele wird der Einstieg in die verschiedenen Wege der Vorauslegung von Triebwerken uns dessen Komponenten eröffnet. Neu hinzugekommen ist ein Kapitel über Propeller- und Propellersysteme.

Advanced Aircraft Design

Author: Egbert Torenbeek
Publisher: John Wiley & Sons
ISBN: 1118568095
Size: 21.50 MB
Format: PDF, Mobi
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Although the overall appearance of modern airliners has not changed a lot since the introduction of jetliners in the 1950s, their safety, efficiency and environmental friendliness have improved considerably. Main contributors to this have been gas turbine engine technology, advanced materials, computational aerodynamics, advanced structural analysis and on-board systems. Since aircraft design became a highly multidisciplinary activity, the development of multidisciplinary optimization (MDO) has become a popular new discipline. Despite this, the application of MDO during the conceptual design phase is not yet widespread. Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes presents a quasi-analytical optimization approach based on a concise set of sizing equations. Objectives are aerodynamic efficiency, mission fuel, empty weight and maximum takeoff weight. Independent design variables studied include design cruise altitude, wing area and span and thrust or power loading. Principal features of integrated concepts such as the blended wing and body and highly non-planar wings are also covered. The quasi-analytical approach enables designers to compare the results of high-fidelity MDO optimization with lower-fidelity methods which need far less computational effort. Another advantage to this approach is that it can provide answers to “what if” questions rapidly and with little computational cost. Key features: Presents a new fundamental vision on conceptual airplane design optimization Provides an overview of advanced technologies for propulsion and reducing aerodynamic drag Offers insight into the derivation of design sensitivity information Emphasizes design based on first principles Considers pros and cons of innovative configurations Reconsiders optimum cruise performance at transonic Mach numbers Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes advances understanding of the initial optimization of civil airplanes and is a must-have reference for aerospace engineering students, applied researchers, aircraft design engineers and analysts.

The Cutting Edge

Author: Mark A. Lorell
Publisher: Rand Corporation
ISBN: 0833048600
Size: 59.36 MB
Format: PDF, Kindle
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The proposition that innovation is critical in the cost-effective design and development of successful military aircraft is still subject to some debate. RAND research indicates that innovation is promoted by intense competition among three or more industry competitors. Given the critical policy importance of this issue in the current environment of drastic consolidation of the aerospace defense industry, the authors here examine the history of the major prime contractors in developing jet fighters since World War II. They make use of an extensive RAND database that includes nearly all jet fighters, fighter-attack aircraft, and bombers developed and flown by U.S. industry since 1945, as well as all related prototypes, modifications, upgrades, etc. The report concludes that (1) experience matters, because of the tendency to specialize and thus to develop system-specific expertise; (2) yet the most dramatic innovations and breakthroughs came from secondary or marginal players trying to compete with the industry leaders; and (3) dedicated military R&D conducted or directly funded by the U.S. government has been critical in the development of new higher-performance fighters and bombers.

Axiomatic Design

Author: René Fiege
Publisher: Springer-Verlag
ISBN: 9783834921369
Size: 79.52 MB
Format: PDF, ePub
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René Fiege adaptiert die aus dem Maschinenbau stammende Methode Axiomatic Design für die Modellierung von serviceorientierten Architekturen. Er zeigt, dass die Methode die erforderlichen Architekturprinzipien stärker fördern kann als alternative Modellierungsmethoden für SOA.