High Angle of Attack Aerodynamics: Subsonic, Transonic, and Supersonic Flows
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Elektronisch E-Book |
| Sprache: | English |
| Veröffentlicht: |
New York, NY
Springer New York
1992
|
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Beschreibung: | The aerodynamics of aircraft at high angles of attack is a subject which is being pursued diligently, because the modern agile fighter aircraft and many of the current generation of missiles must perform well at very high incidence, near and beyond stall. However, a comprehensive presentation of the methods and results applicable to the studies of the complex aerodynamics at high angle of attack has not been covered in monographs or textbooks. This book is not the usual textbook in that it goes beyond just presenting the basic theoretical and experimental know-how, since it contains reference material to practical calculation methods and technical and experimental results which can be useful to the practicing aerospace engineers and scientists. It can certainly be used as a text and reference book for graduate courses on subjects related to high angles of attack aerodynamics and for topics related to three-dimensional separation in viscous flow courses. In addition, the book is addressed to the aerodynamicist interested in a comprehensive reference to methods of analysis and computations of high angle of attack flow phenomena and is written for the aerospace scientist and engineer who is familiar with the basic concepts of viscous and inviscid flows and with computational methods used in fluid dynamics |
| Beschreibung: | 1 Online-Ressource (XIII, 399p. 289 illus) |
| ISBN: | 9781461228240 9781461276869 |
| DOI: | 10.1007/978-1-4612-2824-0 |
Internformat
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| dewey-full | 533.62 532 |
| dewey-hundreds | 500 - Natural sciences and mathematics |
| dewey-ones | 533 - Pneumatics (Gas mechanics) 532 - Fluid mechanics |
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| dewey-sort | 3533.62 |
| dewey-tens | 530 - Physics |
| discipline | Physik |
| doi_str_mv | 10.1007/978-1-4612-2824-0 |
| format | Electronic eBook |
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| spelling | Rom, Josef Verfasser aut High Angle of Attack Aerodynamics Subsonic, Transonic, and Supersonic Flows by Josef Rom New York, NY Springer New York 1992 1 Online-Ressource (XIII, 399p. 289 illus) txt rdacontent c rdamedia cr rdacarrier The aerodynamics of aircraft at high angles of attack is a subject which is being pursued diligently, because the modern agile fighter aircraft and many of the current generation of missiles must perform well at very high incidence, near and beyond stall. However, a comprehensive presentation of the methods and results applicable to the studies of the complex aerodynamics at high angle of attack has not been covered in monographs or textbooks. This book is not the usual textbook in that it goes beyond just presenting the basic theoretical and experimental know-how, since it contains reference material to practical calculation methods and technical and experimental results which can be useful to the practicing aerospace engineers and scientists. It can certainly be used as a text and reference book for graduate courses on subjects related to high angles of attack aerodynamics and for topics related to three-dimensional separation in viscous flow courses. In addition, the book is addressed to the aerodynamicist interested in a comprehensive reference to methods of analysis and computations of high angle of attack flow phenomena and is written for the aerospace scientist and engineer who is familiar with the basic concepts of viscous and inviscid flows and with computational methods used in fluid dynamics Physics Engineering Astronautics Fluid- and Aerodynamics Aerospace Technology and Astronautics Classical Continuum Physics Automotive Engineering Ingenieurwissenschaften Flugzeugaerodynamik (DE-588)4135410-2 gnd rswk-swf Anstellwinkel (DE-588)4282304-3 gnd rswk-swf 1\p (DE-588)1071861417 Konferenzschrift 1978 Sandefjord gnd-content Anstellwinkel (DE-588)4282304-3 s Flugzeugaerodynamik (DE-588)4135410-2 s 2\p DE-604 https://doi.org/10.1007/978-1-4612-2824-0 Verlag Volltext 1\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk 2\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk |
| spellingShingle | Rom, Josef High Angle of Attack Aerodynamics Subsonic, Transonic, and Supersonic Flows Physics Engineering Astronautics Fluid- and Aerodynamics Aerospace Technology and Astronautics Classical Continuum Physics Automotive Engineering Ingenieurwissenschaften Flugzeugaerodynamik (DE-588)4135410-2 gnd Anstellwinkel (DE-588)4282304-3 gnd |
| subject_GND | (DE-588)4135410-2 (DE-588)4282304-3 (DE-588)1071861417 |
| title | High Angle of Attack Aerodynamics Subsonic, Transonic, and Supersonic Flows |
| title_auth | High Angle of Attack Aerodynamics Subsonic, Transonic, and Supersonic Flows |
| title_exact_search | High Angle of Attack Aerodynamics Subsonic, Transonic, and Supersonic Flows |
| title_full | High Angle of Attack Aerodynamics Subsonic, Transonic, and Supersonic Flows by Josef Rom |
| title_fullStr | High Angle of Attack Aerodynamics Subsonic, Transonic, and Supersonic Flows by Josef Rom |
| title_full_unstemmed | High Angle of Attack Aerodynamics Subsonic, Transonic, and Supersonic Flows by Josef Rom |
| title_short | High Angle of Attack Aerodynamics |
| title_sort | high angle of attack aerodynamics subsonic transonic and supersonic flows |
| title_sub | Subsonic, Transonic, and Supersonic Flows |
| topic | Physics Engineering Astronautics Fluid- and Aerodynamics Aerospace Technology and Astronautics Classical Continuum Physics Automotive Engineering Ingenieurwissenschaften Flugzeugaerodynamik (DE-588)4135410-2 gnd Anstellwinkel (DE-588)4282304-3 gnd |
| topic_facet | Physics Engineering Astronautics Fluid- and Aerodynamics Aerospace Technology and Astronautics Classical Continuum Physics Automotive Engineering Ingenieurwissenschaften Flugzeugaerodynamik Anstellwinkel Konferenzschrift 1978 Sandefjord |
| url | https://doi.org/10.1007/978-1-4612-2824-0 |
| work_keys_str_mv | AT romjosef highangleofattackaerodynamicssubsonictransonicandsupersonicflows |