Aircraft performance and sizing. Volume I, Fundamentals of aircraft performance
(eBook)

Book Cover
Average Rating
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.

Description

Loading Description...

Also in this Series

Checking series information...

More Like This

Loading more titles like this title...

Reading Recommendations & More

Reviews from GoodReads

Loading GoodReads Reviews.

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
Go To Grouped Work

Grouping Information

Grouped Work ID9de23d8c-07a4-07f2-6f41-835bd0bafadb-eng
Full titleaircraft performance and sizing volume i fundamentals of aircraft performance
Authortakahashi timothy
Grouping Categorybook
Last Update2022-06-07 21:23:19PM
Last Indexed2024-05-30 04:33:24AM

Book Cover Information

Image Sourcesyndetics
First LoadedMar 2, 2022
Last UsedMar 2, 2022

Marc Record

First DetectedAug 09, 2021 01:49:25 PM
Last File Modification TimeNov 22, 2021 09:45:35 AM

MARC Record

LEADER05102nam a2200625 i 4500
001EBC4432251
003MiAaPQ
006m    E |      
007cr cnu||||||||
008160317s2016    nyua   foab   001 0 eng d
020 |a 9781606506844|q electronic
020 |z 9781606506837|q print
035 |a (Sirsi) EBC4432251
035 |a (Sirsi) EBC4432251
035 |a (OCoLC)945612332
040 |a FINmELB|b spa|c FINmELB|e rda
050 4|a TL671.2|b .T252 2016
0820 |a 629.1341|2 23
1001 |a Takahashi, Timothy.,|e author.
24510|a Aircraft performance and sizing.|c Timothy Takahashi.|n Volume I,|p Fundamentals of aircraft performance|h [eBook]/
24630|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
4901 |a Aerospace engineering collection
504 |a Includes bibliographical references and index.
5050 |a 1. Introduction -- 1.1 Defining a clean-sheet design -- 1.2 Aircraft purpose, the explicit requirements -- 1.3 Certification, the implied requirements --
5058 |a 2. Flight mechanics basics -- 2.1 Reference units -- 2.2 Coordinate frames -- 2.3 Standard atmosphere -- 2.4 How pilots actually fly airplanes --
5058 |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 --
5058 |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 --
5058 |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 --
5058 |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.
5061 |a Restricted to libraries which purchase an unrestricted PDF download via an IP.
5203 |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.
77608|i Print version:|z 9781606506837
830 0|a Aerospace engineering collection.
85640|u http://ebookcentral.proquest.com/lib/yavapai-ebooks/detail.action?docID=4432251|x Yavapai College|y Yavapai College users click here to access
85640|u http://ebookcentral.proquest.com/lib/prescottcollege-ebooks/detail.action?docID=4432251|x Prescott College|y Prescott College users click here to access
85640|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