Advanced multifunctional lightweight aerostructures : design, development, and implementation / / Kamran Behdinan and Rasool Moradi-Dastjerdi |
Autore | Behdinan Kamran <1961-> |
Pubbl/distr/stampa | Hoboken, New Jersey : , : Wiley, , [2021] |
Descrizione fisica | 1 online resource (259 pages) |
Disciplina | 629.1341 |
Collana | Wiley-ASME Press Series |
Soggetto topico |
Airplanes - Design and construction
Lightweight construction Aerospace engineering |
Soggetto genere / forma | Electronic books. |
ISBN |
1-119-75672-3
1-119-75674-X 1-119-75673-1 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910555269603321 |
Behdinan Kamran <1961->
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Hoboken, New Jersey : , : Wiley, , [2021] | ||
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Lo trovi qui: Univ. Federico II | ||
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Advanced multifunctional lightweight aerostructures : design, development, and implementation / / Kamran Behdinan and Rasool Moradi-Dastjerdi |
Autore | Behdinan Kamran <1961-> |
Pubbl/distr/stampa | Hoboken, New Jersey : , : Wiley, , [2021] |
Descrizione fisica | 1 online resource (259 pages) |
Disciplina | 629.1341 |
Collana | Wiley-ASME Press Series |
Soggetto topico |
Airplanes - Design and construction
Lightweight construction Aerospace engineering |
ISBN |
1-5231-5512-4
1-119-75672-3 1-119-75674-X 1-119-75673-1 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910830993503321 |
Behdinan Kamran <1961->
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Hoboken, New Jersey : , : Wiley, , [2021] | ||
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Lo trovi qui: Univ. Federico II | ||
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Aerodinamica applicata al volo : generalità sui fluidi e sul loro movimento ... / Gian Battista Nicolò ; prefazione di A. Eula |
Autore | Nicolò, Gian Battista |
Pubbl/distr/stampa | Roma : Associazione culturale aeronautica, 1950 |
Descrizione fisica | 333 p. : ill. ; 23 cm |
Disciplina |
629.1341
533.62 |
Soggetto non controllato |
Aerodinamica - Applicazioni
Volo - Aerodinamica |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | ita |
Record Nr. | UNINA-990000052440403321 |
Nicolò, Gian Battista
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Roma : Associazione culturale aeronautica, 1950 | ||
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Lo trovi qui: Univ. Federico II | ||
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Aerospace structures and materials / / edited by Yucheng Liu |
Pubbl/distr/stampa | Sharjah, United Arab Emirates : , : Bentham eBooks, , 2016 |
Descrizione fisica | 1 online resource (591 pages) : illustrations |
Disciplina | 629.1341 |
Collana | Frontiers in Aerospace Science |
Soggetto topico |
Airplanes - Design and construction
Space vehicles - Materials |
ISBN | 1-68108-305-1 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910798890603321 |
Sharjah, United Arab Emirates : , : Bentham eBooks, , 2016 | ||
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Lo trovi qui: Univ. Federico II | ||
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Aerospace structures and materials / / edited by Yucheng Liu |
Pubbl/distr/stampa | Sharjah, United Arab Emirates : , : Bentham eBooks, , 2016 |
Descrizione fisica | 1 online resource (591 pages) : illustrations |
Disciplina | 629.1341 |
Collana | Frontiers in Aerospace Science |
Soggetto topico |
Airplanes - Design and construction
Space vehicles - Materials |
ISBN | 1-68108-305-1 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910809038403321 |
Sharjah, United Arab Emirates : , : Bentham eBooks, , 2016 | ||
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Lo trovi qui: Univ. Federico II | ||
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Aircraft design : a conceptual approach / Daniel P. Raymer |
Autore | Raymer, Daniel P. |
Edizione | [5th ed.] |
Pubbl/distr/stampa | Reston (Virginia) : AIAA Education Series, 2012 |
Descrizione fisica | XXVIII, 1044 p. : ill. ; 24 cm |
Disciplina | 629.1341 |
Soggetto non controllato |
Aeroplani - Disegno
Aeroplani - Costruzione |
ISBN | 978-1-60086-911-2 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-990009643030403321 |
Raymer, Daniel P.
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Reston (Virginia) : AIAA Education Series, 2012 | ||
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Lo trovi qui: Univ. Federico II | ||
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Aircraft design projects [e-book] : for engineering students / Lloyd R. Jenkinson, James F. Marchman III |
Autore | Jenkinson, Lloyd R. |
Pubbl/distr/stampa | Oxford ; Boston : Butterworth-Heinemann, 2003 |
Descrizione fisica | xx, 371 p. : ill. ; 25 cm |
Disciplina | 629.1341 |
Altri autori (Persone) | Marchman, James F. |
Soggetto topico | Airplanes - Design and construction |
Soggetto genere / forma | Electronic books. |
ISBN |
9780750657723
0750657723 |
Formato | Risorse elettroniche ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Preface; Acknowledgements; Introduction; Design methodology; Preliminary design; Introduction to the project studies; Project study - scheduled long-range business jet; Project study - military training system; Project study - electric-powered racing aircraft; Project study - advanced deep interdiction aircraft; Project study - high-altitude, long-endurance (HALE) uninhabited aerial surveillance vehicle (UASV); Project study - a general aviation amphibian aircraft; Design organization and presentation; Appendices; Index |
Record Nr. | UNISALENTO-991003225449707536 |
Jenkinson, Lloyd R.
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Oxford ; Boston : Butterworth-Heinemann, 2003 | ||
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Lo trovi qui: Univ. del Salento | ||
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Aircraft performance and design / John D. Anderson Jr. |
Autore | Anderson, John D. <Jr.> |
Pubbl/distr/stampa | Boston : WCB/McGraw-Hill, 1999 |
Descrizione fisica | XVI, 580 p. : ill. ; 24 cm |
Disciplina | 629.1341 |
Collana | Aerospace science. Technology series |
Soggetto non controllato | Aeroplani - Costruzione - Disegno |
ISBN | 0-07-116010-8 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-990009641310403321 |
Anderson, John D. <Jr.>
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Boston : WCB/McGraw-Hill, 1999 | ||
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Lo trovi qui: Univ. Federico II | ||
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Aircraft performance and sizing . Volume I : fundamentals of aircraft performance / / Timothy Takahashi |
Autore | Takahashi Timothy |
Pubbl/distr/stampa | New York, NY : , : Momentum Press, , [2018] |
Descrizione fisica | 1 online resource (xvi, 230 pages) : illustrations |
Disciplina | 629.1341 |
Collana | Aerospace engineering collection |
Soggetto topico |
Airplanes - Design and construction
Airplanes - Performance |
Soggetto genere / forma | Electronic books. |
ISBN | 1-60650-684-6 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
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. |
Record Nr. | UNINA-9910465946303321 |
Takahashi Timothy
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New York, NY : , : Momentum Press, , [2018] | ||
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Lo trovi qui: Univ. Federico II | ||
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Aircraft performance and sizing . Volume I : fundamentals of aircraft performance / / Timothy Takahashi |
Autore | Takahashi Timothy |
Pubbl/distr/stampa | New York, NY : , : Momentum Press, , [2018] |
Descrizione fisica | 1 online resource (xvi, 230 pages) : illustrations |
Disciplina | 629.1341 |
Collana | Aerospace engineering collection |
Soggetto topico |
Airplanes - Design and construction
Airplanes - Performance |
ISBN | 1-60650-684-6 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
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. |
Record Nr. | UNINA-9910798269903321 |
Takahashi Timothy
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New York, NY : , : Momentum Press, , [2018] | ||
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Lo trovi qui: Univ. Federico II | ||
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