Concept Development of a Mach 3.0 High-speed Civil Transport

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ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Concept Development of a Mach 3.0 High-speed Civil Transport by :

Download or read book Concept Development of a Mach 3.0 High-speed Civil Transport written by and published by . This book was released on 1988 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Concept Development of a Mach 3.0 High-speed Civil Transport

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Publisher :
ISBN 13 :
Total Pages : 58 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Concept Development of a Mach 3.0 High-speed Civil Transport by :

Download or read book Concept Development of a Mach 3.0 High-speed Civil Transport written by and published by . This book was released on 1988 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Concept Development of a Mach 2.4 High-Speed Civil Transport

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Publisher : Independently Published
ISBN 13 : 9781723715136
Total Pages : 34 pages
Book Rating : 4.7/5 (151 download)

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Book Synopsis Concept Development of a Mach 2.4 High-Speed Civil Transport by : National Aeronautics and Space Adm Nasa

Download or read book Concept Development of a Mach 2.4 High-Speed Civil Transport written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-09-14 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: In support of the NASA High-Speed Research Program, a Mach 2.4 high-speed civil transport concept was developed to serve as a baseline for studies to assess advanced technologies required for a feasible year 2005 entry-into-service vehicle. The configuration was designed to carry 251 passengers at Mach 2.4 cruise with a 6500-n.mi. range and operate in the existing world airport structure. The details of the configuration development, aerodynamic design, propulsion system and integration, mass properties, sizing, and mission performance are presented. The baseline configuration has a wing area of 9l00 sq ft and a takeoff gross weight of 614300 lb. The four advanced turbine bypass engines have 39 000 lb thrust with a weight of 9950 lb each, yielding a vehicle takeoff thrust-to-weight ratio of 0.254 and a takeoff wing loading of 67.5 lb/sq ft. The configuration was sized by the 11000-ft takeoff field length requirement and the usable fuel volume limit, which results in a rotation speed of 179 knots and an end-of-mission landing approach velocity of 134 knots.Fenbert, James W. and Ozoroski, Lori P. and Geiselhart, Karl A. and Shields, Elwood W. and McElroy, Marcus O.Langley Research CenterSUPERSONIC SPEED; HIGH SPEED; SUPERSONIC CRUISE AIRCRAFT RESEARCH; SUPERSONIC TRANSPORTS; SUPERSONIC AIRCRAFT; TRANSPORT AIRCRAFT; AIRCRAFT DESIGN; AERODYNAMIC CONFIGURATIONS; AIRCRAFT CONFIGURATIONS; PROPULSION SYSTEM CONFIGURATIONS; WING LOADING; THRUST-WEIGHT RATIO; TURBINE ENGINES

Concept Development of a Mach 4 High-speed Civil Transport

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (317 download)

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Download or read book Concept Development of a Mach 4 High-speed Civil Transport written by and published by . This book was released on 1990 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Concept Development of a Mach 3. 0 High-Speed Civil Transport

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Author :
Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722316198
Total Pages : 54 pages
Book Rating : 4.3/5 (161 download)

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Book Synopsis Concept Development of a Mach 3. 0 High-Speed Civil Transport by : National Aeronautics and Space Administration (NASA)

Download or read book Concept Development of a Mach 3. 0 High-Speed Civil Transport written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-08 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt: A baseline concept for a Mach 3.0 high-speed civil transport concept was developed as part of a national program with the goal that concepts and technologies be developed which will enable an effective long-range high-speed civil transport system. The Mach 3.0 concept reported represents an aggressive application of advanced technology to achieve the design goals. The level of technology is generally considered to be that which could have a demonstrated availability date of 1995 to 2000. The results indicate that aircraft are technically feasible that could carry 250 passengers at Mach 3.0 cruise for a 6500 nautical mile range at a size, weight and performance level that allows it to fit into the existing world airport structure. The details of the configuration development, aerodynamic design, propulsion system design and integration, mass properties, mission performance, and sizing are presented. Robins, A. Warner and Dollyhigh, Samuel M. and Beissner, Fred L., Jr. and Geiselhart, Karl and Martin, Glenn L. and Shields, E. W. and Swanson, E. E. and Coen, Peter G. and Morris, Shelby J., Jr. Langley Research Center...

Concept Development of a Mach 4 High-Speed Civil Transport

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722123499
Total Pages : 34 pages
Book Rating : 4.1/5 (234 download)

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Book Synopsis Concept Development of a Mach 4 High-Speed Civil Transport by : National Aeronautics and Space Administration (NASA)

Download or read book Concept Development of a Mach 4 High-Speed Civil Transport written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study was conducted to configure and analyze a 250 passenger, Mach 4 High Speed Civil Transport with a design range of 6500 n.mi. The design mission assumed an all-supersonic cruise segment and no community noise or sonic boom constraints. The study airplane was developed in order to examine the technology requirements for such a vehicle and to provide an unconstrained baseline from which to assess changes in technology levels, sonic boom limits, or community noise constraints in future studies. The propulsion, structure, and materials technologies utilized in the sizing of the study aircraft were assumed to represent a technology availability date of 2015. The study airplane was a derivative of a previously developed Mach 3 concept and utilized advanced afterburning turbojet engines and passive airframe thermal protection. Details of the configuration development, aerodynamic design, propulsion system, mass properties, and mission performance are presented. The study airplane was estimated to weigh approx. 866,000 lbs. Although an aircraft of this size is a marginally acceptable candidate to fit into the world airport infrastructure, it was concluded that the inclusion of community noise or sonic boom constraints would quickly cause the aircraft to grow beyond acceptable limits using the assumed technology levels. Domack, Christopher S. and Dollyhigh, Samuel M. and Beissner, Fred L., Jr. and Geiselhart, Karl A. and Mcgraw, Marvin E., Jr. and Shields, Elwood W. and Swanson, Edward E. Langley Research Center RTOP 505-69-01-02...

Concept Development of a Mach 1. 6 High-Speed Civil Transport

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781721202379
Total Pages : 40 pages
Book Rating : 4.2/5 (23 download)

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Book Synopsis Concept Development of a Mach 1. 6 High-Speed Civil Transport by : National Aeronautics and Space Administration (NASA)

Download or read book Concept Development of a Mach 1. 6 High-Speed Civil Transport written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-15 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: A high-speed civil transport configuration with a Mach number of 1.6 was developed as part of the NASA High-Speed Research Program to serve as a baseline for assessing advanced technologies required for an aircraft with a service entry date of 2005. This configuration offered more favorable solutions to environmental concerns than configurations with higher Mach numbers. The Mach 1.6 configuration was designed for a 6500 n.mi. mission with a 250-passenger payload. The baseline configuration has a wing area of 8732 square feet a takeoff gross weight of 591570 lb, and four 41000-lb advanced turbine bypass engines defined by NASA. These engines have axisymmetric mixer-ejector nozzles that are assumed to yield 20 dB of noise suppression during takeoff, which is assumed to satisfy, the FAR Stage III noise requirements. Any substantial reduction in this assumed level of suppression would require oversizing the engines to meet community noise regulations and would severly impact the gross weight of the aircraft at takeoff. These engines yield a ratio of takeoff thrust to weight of 0.277 and a takeoff wing loading of 67.8 lb/square feet that results in a rotation speed of 169 knots. The approach velocity of the sized configuration at the end of the mission is 131 knots. The baseline configuration was resized with an engine having a projected life of 9000 hr for hot rotating parts and 18000 hr for the rest of the engine, as required for commercial use on an aircraft with a service entry date of 2005. Results show an increase in vehicle takeoff gross weight of approximately 58700 lb. This report presents the details of the configuration development, mass properties, aerodynamic design, propulsion system and integration, mission performance, and sizing. Shields, Elwood W. and Fenbert, James W. and Ozoroski, Lori P. and Geiselhart, Karl A. Langley Research Center NASA/TP-1999-209697, NAS 1.60:209697, L-17242

High-speed Civil Transport Study. Summary

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Publisher :
ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis High-speed Civil Transport Study. Summary by :

Download or read book High-speed Civil Transport Study. Summary written by and published by . This book was released on 1989 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

New Design Concepts for High Speed Air Transport

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Publisher : Springer
ISBN 13 : 3709126584
Total Pages : 333 pages
Book Rating : 4.7/5 (91 download)

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Book Synopsis New Design Concepts for High Speed Air Transport by : H. Sobieczky

Download or read book New Design Concepts for High Speed Air Transport written by H. Sobieczky and published by Springer. This book was released on 2014-05-04 with total page 333 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book presents the challenges, the tools and the concepts for developing economically viable high speed civil transport aircraft under environmental constraints. Computational tools for aircraft design and optimization are outlined and application in an industrial environment is shown for new and innovative case studies.

Study of High-speed Civil Transports

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Publisher :
ISBN 13 :
Total Pages : 192 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Study of High-speed Civil Transports by : Douglas Aircraft Company. New Commercial Programs

Download or read book Study of High-speed Civil Transports written by Douglas Aircraft Company. New Commercial Programs and published by . This book was released on 1989 with total page 192 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Study of High-speed Civil Transports

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Publisher :
ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Study of High-speed Civil Transports by : Douglas Aircraft Company. New Commercial Programs

Download or read book Study of High-speed Civil Transports written by Douglas Aircraft Company. New Commercial Programs and published by . This book was released on 1990 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

High-speed Civil Transport Study

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Publisher :
ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis High-speed Civil Transport Study by : Boeing Commercial Airplane Company. New Airplane Development Group

Download or read book High-speed Civil Transport Study written by Boeing Commercial Airplane Company. New Airplane Development Group and published by . This book was released on 1989 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalogue, United States Public Documents

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ISBN 13 :
Total Pages : 1636 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Monthly Catalogue, United States Public Documents by :

Download or read book Monthly Catalogue, United States Public Documents written by and published by . This book was released on 1995 with total page 1636 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalog of United States Government Publications

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Publisher :
ISBN 13 :
Total Pages : 882 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis Monthly Catalog of United States Government Publications by :

Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1990 with total page 882 pages. Available in PDF, EPUB and Kindle. Book excerpt:

U.S. Supersonic Commercial Aircraft

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Publisher : National Academies Press
ISBN 13 : 9780309058780
Total Pages : 168 pages
Book Rating : 4.0/5 (587 download)

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Book Synopsis U.S. Supersonic Commercial Aircraft by : National Research Council

Download or read book U.S. Supersonic Commercial Aircraft written by National Research Council and published by National Academies Press. This book was released on 1997-08-25 with total page 168 pages. Available in PDF, EPUB and Kindle. Book excerpt: The National Aeronautics and Space Administration (NASA) is currently developing advanced technologies to form the foundation for the next breakthrough in civil aviation: an economically viable, environmentally acceptable supersonic transport. NASA's High Speed Research Program works in conjunction with industry to identify and address critical technological challenges to initiating commercial development of a practical supersonic transport. The key technical areas investigated are engine emissions, fuel efficiency, service life, and weight; community noise; aircraft range and payload; and weight and service life of airframe structures. Areas of particular interest include the ability of technologies under development to meet program goals related to noise, emissions, service life, weight, range, and payload. This book examines aircraft design requirements, assesses the program's planning and progress, and recommends changes that will help the program achieve its overall objectives.

Control and Dynamic Systems V57: Multidisciplinary Engineering Systems: Design and Optimization Techniques and Their Application

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Publisher : Academic Press
ISBN 13 : 0323163092
Total Pages : 508 pages
Book Rating : 4.3/5 (231 download)

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Book Synopsis Control and Dynamic Systems V57: Multidisciplinary Engineering Systems: Design and Optimization Techniques and Their Application by : C.T. Leonides

Download or read book Control and Dynamic Systems V57: Multidisciplinary Engineering Systems: Design and Optimization Techniques and Their Application written by C.T. Leonides and published by Academic Press. This book was released on 2012-12-02 with total page 508 pages. Available in PDF, EPUB and Kindle. Book excerpt: Control and Dynamic Systems: Advances in Theory and Applications, Volume 57: Multidisciplinary Engineering Systems: Design and Optimization Techniques and their Application deals with techniques used in the design and optimization of future engineering systems. Comprised of 11 chapters, this book covers techniques for improving product design quality in multidisciplinary systems. These techniques include decomposition techniques for synthesis process; optimization for aircraft systems; actuator and sensor placement; and robust techniques in system design and control process. Students, research workers, and practising engineers will find this book invaluable.

Scientific and Technical Aerospace Reports

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Publisher :
ISBN 13 :
Total Pages : 704 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt: