Aircraft performance and sizing. Volume I, Fundamentals of aircraft performance
(eBook)
Author
Published
New York, [New York] (222 East 46th Street, New York, NY 10017) : Momentum Press, 2016.
Physical Desc
1 online resource (xvi, 230 pages) : illustrations.
Status
More Details
Format
eBook
Language
English
ISBN
9781606506844
Notes
Bibliography
Includes bibliographical references and index.
Restrictions on Access
Restricted to libraries which purchase an unrestricted PDF download via an IP.
Description
This book is a concise practical treatise for the student or experienced professional aircraft designer. This volume comprises key fundamental subjects for aerodynamic performance analysis: the basics of flight mechanics bridging both engineering and piloting perspectives, propulsion system performance attributes, practical drag prediction methods, aircraft "up and away" flight performance and aircraft mission performance. This book may serve as a textbook for an undergraduate aircraft performance course or as a reference for the classically trained practicing engineer.
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Citations
APA Citation, 7th Edition (style guide)
Takahashi, T. (2016). Aircraft performance and sizing . Momentum Press.
Chicago / Turabian - Author Date Citation, 17th Edition (style guide)Takahashi, Timothy.. 2016. Aircraft Performance and Sizing. Momentum Press.
Chicago / Turabian - Humanities (Notes and Bibliography) Citation, 17th Edition (style guide)Takahashi, Timothy.. Aircraft Performance and Sizing Momentum Press, 2016.
MLA Citation, 9th Edition (style guide)Takahashi, Timothy.. Aircraft Performance and Sizing Momentum Press, 2016.
Note! Citations contain only title, author, edition, publisher, and year published. Citations should be used as a guideline and should be double checked for accuracy. Citation formats are based on standards as of August 2021.
Staff View
Grouped Work ID
9de23d8c-07a4-07f2-6f41-835bd0bafadb-eng
Grouping Information
Grouped Work ID | 9de23d8c-07a4-07f2-6f41-835bd0bafadb-eng |
---|---|
Full title | aircraft performance and sizing volume i fundamentals of aircraft performance |
Author | takahashi timothy |
Grouping Category | book |
Last Update | 2022-06-07 21:23:19PM |
Last Indexed | 2024-05-30 04:33:24AM |
Book Cover Information
Image Source | syndetics |
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First Loaded | Mar 2, 2022 |
Last Used | Mar 2, 2022 |
Marc Record
First Detected | Aug 09, 2021 01:49:25 PM |
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Last File Modification Time | Nov 22, 2021 09:45:35 AM |
MARC Record
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020 | |a 9781606506844|q electronic | ||
020 | |z 9781606506837|q print | ||
035 | |a (Sirsi) EBC4432251 | ||
035 | |a (Sirsi) EBC4432251 | ||
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050 | 4 | |a TL671.2|b .T252 2016 | |
082 | 0 | |a 629.1341|2 23 | |
100 | 1 | |a Takahashi, Timothy.,|e author. | |
245 | 1 | 0 | |a Aircraft performance and sizing.|c Timothy Takahashi.|n Volume I,|p Fundamentals of aircraft performance|h [eBook]/ |
246 | 3 | 0 | |a Fundamentals of aircraft performance. |
264 | 1 | |a New York, [New York] (222 East 46th Street, New York, NY 10017) :|b Momentum Press,|c 2016. | |
300 | |a 1 online resource (xvi, 230 pages) :|b illustrations. | ||
336 | |a text|2 rdacontent | ||
337 | |a computer|2 rdamedia | ||
338 | |a online resource|2 rdacarrier | ||
490 | 1 | |a Aerospace engineering collection | |
504 | |a Includes bibliographical references and index. | ||
505 | 0 | |a 1. Introduction -- 1.1 Defining a clean-sheet design -- 1.2 Aircraft purpose, the explicit requirements -- 1.3 Certification, the implied requirements -- | |
505 | 8 | |a 2. Flight mechanics basics -- 2.1 Reference units -- 2.2 Coordinate frames -- 2.3 Standard atmosphere -- 2.4 How pilots actually fly airplanes -- | |
505 | 8 | |a 3. Propulsion system design drivers and performance -- 3.1 Gas turbine fundamentals -- 3.2 Calculating thrust and fuel flow -- 3.3 Propulsion system components and design drivers -- 3.4 Example engine performance data -- | |
505 | 8 | |a 4. Aerodynamic analysis fundamentals: lift and drag -- 4.1 Full configuration drag estimation -- 4.2 Zero-lift drag at incompressible speeds -- 4.3 Zero-lift drag due to compressibility -- 4.4 Drag due to lift at incompressible speeds -- 4.5 Drag due to lift arising from compressibility -- 4.6 "Crud drag," the drag of real versus idealized aerostructures -- 4.7 Maximum lift coefficient/buffet boundary -- 4.8 Angle of attack -- 4.9 Take-off, approach, and landing aerodynamics -- | |
505 | 8 | |a 5. Kinematic "point-performance" principles -- 5.1 Standard atmosphere revisited -- 5.2 Computing stall speed -- 5.3 Minimum and maximum permissible flight speeds -- 5.4 The energy-maneuverability skymap plot -- 5.5 Inferring lift and drag in an E-M plot -- 5.6 Aerodynamic efficiency (L/D) and performance efficiency (M(L/D)) -- 5.7 Dimensionalizing drag -- 5.8 Propulsive performance -- 5.9 Specific excess thrust and linear acceleration capability -- 5.10 Specific excess power, rate of climb (R.O.C.), and ceiling -- 5.11 Specific range -- 5.12 Loiter -- 5.13 Induced drag fraction of total drag for level flight limited by aerodynamics and propulsion -- 5.14 Maximum load factor, instantaneous turn rate and stall speed ratio -- 5.15 Combat agility, maximum sustained turn rate -- | |
505 | 8 | |a 6. Mission performance principles -- 6.1 Breguet range equation -- 6.2 Time-step integrating simulations -- 6.3 Creating missions using a mission simulation code -- 6.4 Observations examining the output of a mission simulation code -- 6.5 Creating trade studies using a mission simulation code -- 6.6 Creating payload/range charts using a mission simulation code -- Index. | |
506 | 1 | |a Restricted to libraries which purchase an unrestricted PDF download via an IP. | |
520 | 3 | |a This book is a concise practical treatise for the student or experienced professional aircraft designer. This volume comprises key fundamental subjects for aerodynamic performance analysis: the basics of flight mechanics bridging both engineering and piloting perspectives, propulsion system performance attributes, practical drag prediction methods, aircraft "up and away" flight performance and aircraft mission performance. This book may serve as a textbook for an undergraduate aircraft performance course or as a reference for the classically trained practicing engineer. | |
588 | |a Title from PDF title page (viewed on March 17, 2016). | ||
650 | 0 | |a Airplanes|x Design and construction. | |
650 | 0 | |a Airplanes|x Performance. | |
653 | |a Aerodynamics | ||
653 | |a Aircraft Design | ||
653 | |a Aircraft Performance | ||
653 | |a Aircraft Sizing, | ||
653 | |a Drag | ||
653 | |a Lift | ||
653 | |a Aircraft Stability | ||
653 | |a Aircraft Control | ||
653 | |a Aviation | ||
655 | 4 | |a Libros electronicos. | |
776 | 0 | 8 | |i Print version:|z 9781606506837 |
830 | 0 | |a Aerospace engineering collection. | |
856 | 4 | 0 | |u http://ebookcentral.proquest.com/lib/yavapai-ebooks/detail.action?docID=4432251|x Yavapai College|y Yavapai College users click here to access |
856 | 4 | 0 | |u http://ebookcentral.proquest.com/lib/prescottcollege-ebooks/detail.action?docID=4432251|x Prescott College|y Prescott College users click here to access |
856 | 4 | 0 | |u http://ebookcentral.proquest.com/lib/yln-ebooks/detail.action?docID=4432251|x Yavapai Library Network|y All other users click here to access |
945 | |a E-Book |