Synergistic Airframe Propulsion Interactions And Integrations

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Synergistic Airframe-propulsion Interactions and Integrations

Anonim
Synergistic Airframe propulsion Interactions and Integrations Book PDF

Author : Anonim
Publisher : Unknown
Page : 128 pages
File Size : 43,8 Mb
Release : 1998
Category : Airframes
ISBN : NASA:31769000629181

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Synergistic Airframe-propulsion Interactions and Integrations by Anonim Pdf

This white paper addresses the subject of Synergistic Airframe-Propulsion interactions and integrations (SnAPII). The benefits of SnAPII have not been as extensively explored. This is due primarily to the separateness of design process for airframes and propulsion systems, with only unfavorable interactions addressed. The question "How to design these two systems in such a way that the airframe needs the propulsion and the propulsion needs the airframe?" is the fundamental issue addressed in this paper. Successful solutions to this issue depend on appropriate technology ideas. This paper first details some ten technologies that have yet to make it to commercial products (with limited exceptions) and that could be utilized in a synergistic manner. Then these technologies, either alone or in combination, are applied to both a conventioal two-engine transonic transport and to an unconventional transport, the Blended Wing Body. Lastly, combinations of these technologies are applied to configuration concepts to assess the possibilities of success relative to five of the ten NASA aeronautics goals. These assessments are subjective, but they point the way in which the applied technologies could work together for some break-through benefits.

Power-Based Study of Boundary Layer Ingestion for Aircraft Application

Peijian Lv
Power Based Study of Boundary Layer Ingestion for Aircraft Application Book PDF

Author : Peijian Lv
Publisher : Springer Nature
Page : 138 pages
File Size : 47,7 Mb
Release : 2022-09-14
Category : Technology & Engineering
ISBN : 9789811954979

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Power-Based Study of Boundary Layer Ingestion for Aircraft Application by Peijian Lv Pdf

This book presents research on Boundary Layer Ingestion (BLI). BLI is an aircraft-engine integration technique that aims at integrating the aircraft and the propulsion system such that the overall aircraft fuel consumption can be reduced. In this research, theoretical analysis suggests that the minimization of total power consumption should be used as a design criterion for aircraft utilizing BLI rather than focusing on the minimization of drag. Numerical simulations are performed, and the simulation results are processed using the PBM to support the theoretical analysis. Furthermore, an experimental study is carried out with a focus on the power conversion processes involved for a propulsor operating in the wake. Stereoscopic PIV is employed in order to visualize the flow and understand the physics. The so-called Power-based Method is used to quantify the power conversion mechanisms. The results prove that the dominant mechanism responsible for the efficiency enhancement is due to the utilization of body wake energy by the wake ingesting propeller. In short, the importance of wake energy flow rate in understanding the BLI phenomenon is highlighted. This book will be useful for researchers in the field of aircraft propulsion, aircraft aerodynamics, and airframe propulsion integration.

Stability and Control of Conventional and Unconventional Aerospace Vehicle Configurations

Bernd Chudoba
Stability and Control of Conventional and Unconventional Aerospace Vehicle Configurations Book PDF

Author : Bernd Chudoba
Publisher : Springer
Page : 392 pages
File Size : 48,9 Mb
Release : 2019-07-23
Category : Technology & Engineering
ISBN : 9783030168568

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Stability and Control of Conventional and Unconventional Aerospace Vehicle Configurations by Bernd Chudoba Pdf

This book introduces a stability and control methodology named AeroMech, capable of sizing the primary control effectors of fixed wing subsonic to hypersonic designs of conventional and unconventional configuration layout. Control power demands are harmonized with static-, dynamic-, and maneuver stability requirements, while taking the six-degree-of-freedom trim state into account. The stability and control analysis solves the static- and dynamic equations of motion combined with non-linear vortex lattice aerodynamics for analysis. The true complexity of addressing subsonic to hypersonic vehicle stability and control during the conceptual design phase is hidden in the objective to develop a generic (vehicle configuration independent) methodology concept. The inclusion of geometrically asymmetric aircraft layouts, in addition to the reasonably well-known symmetric aircraft types, contributes significantly to the overall technical complexity and level of abstraction. The first three chapters describe the preparatory work invested along with the research strategy devised, thereby placing strong emphasis on systematic and thorough knowledge utilization. The engineering-scientific method itself is derived throughout the second half of the book. This book offers a unique aerospace vehicle configuration independent (generic) methodology and mathematical algorithm. The approach satisfies the initial technical quest: How to develop a ‘configuration stability & control’ methodology module for an advanced multi-disciplinary aerospace vehicle design synthesis environment that permits consistent aerospace vehicle design evaluations?

Advanced Aircraft Design

Egbert Torenbeek
Advanced Aircraft Design Book PDF

Author : Egbert Torenbeek
Publisher : John Wiley & Sons
Page : 412 pages
File Size : 44,8 Mb
Release : 2013-05-28
Category : Technology & Engineering
ISBN : 9781118568095

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Advanced Aircraft Design by Egbert Torenbeek Pdf

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.

Fundamentals of High Lift for Future Civil Aircraft

Rolf Radespiel,Richard Semaan
Fundamentals of High Lift for Future Civil Aircraft Book PDF

Author : Rolf Radespiel,Richard Semaan
Publisher : Springer Nature
Page : 634 pages
File Size : 46,7 Mb
Release : 2020-10-17
Category : Technology & Engineering
ISBN : 9783030524296

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Fundamentals of High Lift for Future Civil Aircraft by Rolf Radespiel,Richard Semaan Pdf

This book reports on the latest numerical and experimental findings in the field of high-lift technologies. It covers interdisciplinary research subjects relating to scientific computing, aerodynamics, aeroacoustics, material sciences, aircraft structures, and flight mechanics. The respective chapters are based on papers presented at the Final Symposium of the Collaborative Research Center (CRC) 880, which was held on December 17-18, 2019 in Braunschweig, Germany. The conference and the research presented here were partly supported by the CRC 880 on “Fundamentals of High Lift for Future Civil Aircraft,” funded by the DFG (German Research Foundation). The papers offer timely insights into high-lift technologies for short take-off and landing aircraft, with a special focus on aeroacoustics, efficient high-lift, flight dynamics, and aircraft design.

New Results in Numerical and Experimental Fluid Mechanics IV

Christian Breitsamter,Boris Laschka,Hans-Joachim Heinemann,Reinhard Hilbig
New Results in Numerical and Experimental Fluid Mechanics IV Book PDF

Author : Christian Breitsamter,Boris Laschka,Hans-Joachim Heinemann,Reinhard Hilbig
Publisher : Springer Science & Business Media
Page : 497 pages
File Size : 47,9 Mb
Release : 2012-08-13
Category : Technology & Engineering
ISBN : 9783540396048

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New Results in Numerical and Experimental Fluid Mechanics IV by Christian Breitsamter,Boris Laschka,Hans-Joachim Heinemann,Reinhard Hilbig Pdf

This volume contains 59 papers presented at the 13th Symposium of STAB (German Aerospace Aerodynamics Association). In this association, all those German scientists and engineers from universities, research establishments and industry are involved who are doing research and project work in numerical and experimental fluid mechanics and aerodynamics, mainly for aerospace but also in other applications. Many of the contributions give results from federal and European-Union sponsored projects. The volume gives a broad overview of the ongoing work in this field in Germany. Covered are flow problems of high and low aspect-ratio wings and bluff bodies, laminar flow control and transition, hypersonic flows, transition and fluid mechanical modelling, LES and DNS, numerical simulation, aeroelasticity, measuring techniques and propulsion flows.

Hermann Schlichting – 100 Years

Rolf Radespiel,Cord-Christian Rossow,Benjamin Winfried Brinkmann
Hermann Schlichting 100 Years Book PDF

Author : Rolf Radespiel,Cord-Christian Rossow,Benjamin Winfried Brinkmann
Publisher : Springer Science & Business Media
Page : 202 pages
File Size : 40,7 Mb
Release : 2009-03-06
Category : Technology & Engineering
ISBN : 9783540959984

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Hermann Schlichting – 100 Years by Rolf Radespiel,Cord-Christian Rossow,Benjamin Winfried Brinkmann Pdf

Hermann Schlichting is one of the internationally leading scientists in the field of th fluid mechanics during the 20 century. He contributed largely to modern theories of viscous flows and aircraft aerodynamics. His famous monographies Boundary Layer Theory and Aerodynamics of Aircraft are known worldwide and they appeared in six languages. He held Chairs of Aerodynamics and Fluid Mechanics at Technische U- versität Braunschweig during 37 years and directed the Institute of Aerodynamics of the Deutsche Forschungsanstalt für Luftfahrt in Braunschweig. He also directed the Aerodynamische Versuchsanstalt Göttingen and served in the Executive Board of the German Aerospace Center (DFVLR). Hermann Schlichting played a leading role in the rebuilding of aerospace research in Germany after the Second World War. th The occasion of his 100 birthday in the year 2007 was an excellent opportunity to acknowledge important ideas and accomplishments that Hermann Schlichting c- tributed to science. The editors of this volume are the present successors of Hermann Schlichting in his role as director of the two research institutes in Braunschweig. We were glad to host a scientific colloquium in his honor on 28 September 2007. Invited former scholars of Hermann Schlichting reviewed his work in boundary layer theory and in aircraft aerodynamics followed by presentations of important research results of his institutes today.

Active Flow and Combustion Control 2018

Rudibert King
Active Flow and Combustion Control 2018 Book PDF

Author : Rudibert King
Publisher : Springer
Page : 380 pages
File Size : 45,6 Mb
Release : 2018-09-03
Category : Technology & Engineering
ISBN : 9783319981772

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Active Flow and Combustion Control 2018 by Rudibert King Pdf

The book reports on the latest theoretical and experimental findings in the field of active flow and combustion control. It covers new developments in actuator technology and sensing, in robust and optimal open- and closed-loop control, as well as in model reduction for control, constant volume combustion and dynamic impingement cooling. The chapters reports oncutting-edge contributions presented during the fourth edition of the Active Flow and Combustion Control conference, held in September 19 to 21, 2018 at the Technische Universität Berlin, in Germany. This conference, as well as the research presented in the book, have been supported by the collaborative research center SFB 1029 on “Substantial efficiency increase in gas turbines through direct use of coupled unsteady combustion and flow dynamics”, funded by the DFG (German Research Foundation). It offers a timely guide for researchers and practitioners in the field of aeronautics, turbomachinery, control and combustion.

Innovation in Flight

Joseph R. Chambers
Innovation in Flight Book PDF

Author : Joseph R. Chambers
Publisher : Unknown
Page : 406 pages
File Size : 54,6 Mb
Release : 2005
Category : Aeronautics
ISBN : IND:30000109243109

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Innovation in Flight by Joseph R. Chambers Pdf

Active Flow and Combustion Control 2014

Rudibert King
Active Flow and Combustion Control 2014 Book PDF

Author : Rudibert King
Publisher : Springer
Page : 405 pages
File Size : 50,5 Mb
Release : 2014-09-13
Category : Technology & Engineering
ISBN : 9783319119670

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Active Flow and Combustion Control 2014 by Rudibert King Pdf

The book reports on the latest theoretical and experimental advances in the field of active flow and combustion control. It covers new developments in actuator technology and sensing, in robust and optimal open- and closed-loop control, as well as in model reduction for control. It collects contributions presented during the third edition of the Active Flow and Combustion Control conference, held in September 10-12, 2014 at the Technische Universität Berlin (Germany). This conference, as well as the research presented in the book, have been supported by the collaborative research center SFB 1029 -Substantial efficiency increase in gas turbines through direct use of coupled unsteady combustion and flow dynamics, funded by the DFG (German Research Foundation).