Aircraft performance and sizing.: Volume I, Fundamentals of aircraft performance /
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 performa...
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Elektronisch E-Book |
| Sprache: | English |
| Veröffentlicht: |
New York [New York] (222 East 46th Street, New York, NY 10017) :
Momentum Press,
2016.
|
| Schriftenreihe: | Aerospace engineering collection.
|
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Zusammenfassung: | 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. |
| Beschreibung: | Title from PDF title page (viewed on March 17, 2016). |
| Beschreibung: | 1 online resource (1 PDF (xvi, 230 pages)) : illustrations |
| Bibliographie: | Includes bibliographical references and index. |
| ISBN: | 9781606506844 1606506846 1606506838 9781606506837 |
Internformat
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| 100 | 1 | |a Takahashi, Timothy, |d 1966- |e author. |0 http://id.loc.gov/authorities/names/no2016087510 | |
| 245 | 1 | 0 | |a Aircraft performance and sizing. |n Volume I, |p Fundamentals of aircraft performance / |c Timothy Takahashi. |
| 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 (1 PDF (xvi, 230 pages)) : |b illustrations | ||
| 336 | |a text |b txt |2 rdacontent | ||
| 337 | |a electronic |2 isbdmedia | ||
| 338 | |a online resource |b cr |2 rdacarrier | ||
| 490 | 1 | |a Aerospace engineering collection | |
| 500 | |a Title from PDF title page (viewed on March 17, 2016). | ||
| 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. | |
| 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. | |
| 650 | 0 | |a Airplanes |x Design and construction. |0 http://id.loc.gov/authorities/subjects/sh85002801 | |
| 650 | 0 | |a Airplanes |x Performance. |0 http://id.loc.gov/authorities/subjects/sh85002875 | |
| 650 | 6 | |a Avions |x Conception et construction. | |
| 650 | 6 | |a Avions |x Performances. | |
| 650 | 7 | |a TECHNOLOGY & ENGINEERING |x Engineering (General) |2 bisacsh | |
| 650 | 7 | |a Airplanes |x Design and construction |2 fast | |
| 650 | 7 | |a Airplanes |x Performance |2 fast | |
| 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 | ||
| 758 | |i has work: |a Volume 1 Aircraft performance and sizing Fundamentals of aircraft performance (Text) |1 https://id.oclc.org/worldcat/entity/E39PCH94CGPj7Pq3TW4WbffykC |4 https://id.oclc.org/worldcat/ontology/hasWork | ||
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| _version_ | 1816882343260979203 |
| adam_text | |
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| author | Takahashi, Timothy, 1966- |
| author_GND | http://id.loc.gov/authorities/names/no2016087510 |
| author_facet | Takahashi, Timothy, 1966- |
| author_role | aut |
| author_sort | Takahashi, Timothy, 1966- |
| author_variant | t t tt |
| building | Verbundindex |
| bvnumber | localFWS |
| callnumber-first | T - Technology |
| callnumber-label | TL671 |
| callnumber-raw | TL671.2 .T252 2016 |
| callnumber-search | TL671.2 .T252 2016 |
| callnumber-sort | TL 3671.2 T252 42016 |
| callnumber-subject | TL - Motor Vehicles and Aeronautics |
| collection | ZDB-4-EBA |
| contents | 1. Introduction -- 1.1 Defining a clean-sheet design -- 1.2 Aircraft purpose, the explicit requirements -- 1.3 Certification, the implied requirements. 2. Flight mechanics basics -- 2.1 Reference units -- 2.2 Coordinate frames -- 2.3 Standard atmosphere -- 2.4 How pilots actually fly airplanes. 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. 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. 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. 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. |
| ctrlnum | (OCoLC)945180204 |
| dewey-full | 629.1341 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 629 - Other branches of engineering |
| dewey-raw | 629.1341 |
| dewey-search | 629.1341 |
| dewey-sort | 3629.1341 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Verkehr / Transport |
| format | Electronic eBook |
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| id | ZDB-4-EBA-ocn945180204 |
| illustrated | Illustrated |
| indexdate | 2024-11-27T13:27:06Z |
| institution | BVB |
| isbn | 9781606506844 1606506846 1606506838 9781606506837 |
| language | English |
| oclc_num | 945180204 |
| open_access_boolean | |
| owner | MAIN DE-863 DE-BY-FWS |
| owner_facet | MAIN DE-863 DE-BY-FWS |
| physical | 1 online resource (1 PDF (xvi, 230 pages)) : illustrations |
| psigel | ZDB-4-EBA |
| publishDate | 2016 |
| publishDateSearch | 2016 |
| publishDateSort | 2016 |
| publisher | Momentum Press, |
| record_format | marc |
| series | Aerospace engineering collection. |
| series2 | Aerospace engineering collection |
| spelling | Takahashi, Timothy, 1966- author. http://id.loc.gov/authorities/names/no2016087510 Aircraft performance and sizing. Volume I, Fundamentals of aircraft performance / Timothy Takahashi. Fundamentals of aircraft performance New York [New York] (222 East 46th Street, New York, NY 10017) : Momentum Press, 2016. 1 online resource (1 PDF (xvi, 230 pages)) : illustrations text txt rdacontent electronic isbdmedia online resource cr rdacarrier Aerospace engineering collection Title from PDF title page (viewed on March 17, 2016). Includes bibliographical references and index. 1. Introduction -- 1.1 Defining a clean-sheet design -- 1.2 Aircraft purpose, the explicit requirements -- 1.3 Certification, the implied requirements. 2. Flight mechanics basics -- 2.1 Reference units -- 2.2 Coordinate frames -- 2.3 Standard atmosphere -- 2.4 How pilots actually fly airplanes. 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. 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. 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. 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. 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. Airplanes Design and construction. http://id.loc.gov/authorities/subjects/sh85002801 Airplanes Performance. http://id.loc.gov/authorities/subjects/sh85002875 Avions Conception et construction. Avions Performances. TECHNOLOGY & ENGINEERING Engineering (General) bisacsh Airplanes Design and construction fast Airplanes Performance fast Aerodynamics Aircraft Design Aircraft Performance Aircraft Sizing, Drag Lift Aircraft Stability Aircraft Control Aviation has work: Volume 1 Aircraft performance and sizing Fundamentals of aircraft performance (Text) https://id.oclc.org/worldcat/entity/E39PCH94CGPj7Pq3TW4WbffykC https://id.oclc.org/worldcat/ontology/hasWork Print version: 9781606506837 Aerospace engineering collection. FWS01 ZDB-4-EBA FWS_PDA_EBA https://search.ebscohost.com/login.aspx?direct=true&scope=site&db=nlebk&AN=1194405 Volltext |
| spellingShingle | Takahashi, Timothy, 1966- Aircraft performance and sizing. Aerospace engineering collection. 1. Introduction -- 1.1 Defining a clean-sheet design -- 1.2 Aircraft purpose, the explicit requirements -- 1.3 Certification, the implied requirements. 2. Flight mechanics basics -- 2.1 Reference units -- 2.2 Coordinate frames -- 2.3 Standard atmosphere -- 2.4 How pilots actually fly airplanes. 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. 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. 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. 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. Airplanes Design and construction. http://id.loc.gov/authorities/subjects/sh85002801 Airplanes Performance. http://id.loc.gov/authorities/subjects/sh85002875 Avions Conception et construction. Avions Performances. TECHNOLOGY & ENGINEERING Engineering (General) bisacsh Airplanes Design and construction fast Airplanes Performance fast |
| subject_GND | http://id.loc.gov/authorities/subjects/sh85002801 http://id.loc.gov/authorities/subjects/sh85002875 |
| title | Aircraft performance and sizing. |
| title_alt | Fundamentals of aircraft performance |
| title_auth | Aircraft performance and sizing. |
| title_exact_search | Aircraft performance and sizing. |
| title_full | Aircraft performance and sizing. Volume I, Fundamentals of aircraft performance / Timothy Takahashi. |
| title_fullStr | Aircraft performance and sizing. Volume I, Fundamentals of aircraft performance / Timothy Takahashi. |
| title_full_unstemmed | Aircraft performance and sizing. Volume I, Fundamentals of aircraft performance / Timothy Takahashi. |
| title_short | Aircraft performance and sizing. |
| title_sort | aircraft performance and sizing fundamentals of aircraft performance |
| topic | Airplanes Design and construction. http://id.loc.gov/authorities/subjects/sh85002801 Airplanes Performance. http://id.loc.gov/authorities/subjects/sh85002875 Avions Conception et construction. Avions Performances. TECHNOLOGY & ENGINEERING Engineering (General) bisacsh Airplanes Design and construction fast Airplanes Performance fast |
| topic_facet | Airplanes Design and construction. Airplanes Performance. Avions Conception et construction. Avions Performances. TECHNOLOGY & ENGINEERING Engineering (General) Airplanes Design and construction Airplanes Performance |
| url | https://search.ebscohost.com/login.aspx?direct=true&scope=site&db=nlebk&AN=1194405 |
| work_keys_str_mv | AT takahashitimothy aircraftperformanceandsizingvolumei AT takahashitimothy fundamentalsofaircraftperformance |