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Hypersonic curved compression inlet and its inverse design / / Kunyuan Zhang
| Hypersonic curved compression inlet and its inverse design / / Kunyuan Zhang |
| Autore | Zhang Kun-Yuan |
| Edizione | [1st edition 2020.] |
| Pubbl/distr/stampa | Singapore : , : Springer Singapore : , : Imprint : Springer, , 2020 |
| Descrizione fisica | 1 online resource (XIV, 332 p.) : 391 illus., 288 illus. in color |
| Disciplina | 629.132306 |
| Collana | Advanced Topics in Science and Technology in China |
| Soggetto topico |
Aerodynamics, Hypersonic
Curves Fluid- and Aerodynamics Engineering Fluid Dynamics Aerospace Technology and Astronautics |
| ISBN | 981-15-0727-9 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Introduction -- Calculation and Analysis Method of Two Dimensional Curved Shock Wave Curved Compression Flow Field -- Forward Design of Two Dimensional Curved Shock Wave Curved Compression Surface -- Inverse Design of Compression Inlet with Specified Exit Aerodynamic Parameters -- Inverse Design of Curved Shock Wave Compression Surface on Basis of Specified Wall Aerodynamic Parameters -- Inverse Design of Axisymmetric Reference Flow Field on Basis of Specified Wall Aerodynamic Parameters -- Inverse Design and Experiment of Hypersonic Curved Shock Wave Compression Inlet -- Concept of Hypersonic Adaptive Variable Geometric Curved Compression Inlet -- Features and Drag Reduction Analysis of Drag in Hypersonic Inlet -- The Development of Curved Compression and Application Prospect. |
| Record Nr. | UNINA-9910373956303321 |
Zhang Kun-Yuan
|
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| Singapore : , : Springer Singapore : , : Imprint : Springer, , 2020 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Hypersonic curved compression inlet and its inverse design / / Kunyuan Zhang
| Hypersonic curved compression inlet and its inverse design / / Kunyuan Zhang |
| Autore | Zhang Kun-Yuan |
| Edizione | [1st edition 2020.] |
| Pubbl/distr/stampa | Singapore : , : Springer Singapore : , : Imprint : Springer, , 2020 |
| Descrizione fisica | 1 online resource (XIV, 332 p.) : 391 illus., 288 illus. in color |
| Disciplina | 629.132306 |
| Collana | Advanced Topics in Science and Technology in China |
| Soggetto topico |
Aerodynamics, Hypersonic
Curves Fluid- and Aerodynamics Engineering Fluid Dynamics Aerospace Technology and Astronautics |
| ISBN | 981-15-0727-9 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Introduction -- Calculation and Analysis Method of Two Dimensional Curved Shock Wave Curved Compression Flow Field -- Forward Design of Two Dimensional Curved Shock Wave Curved Compression Surface -- Inverse Design of Compression Inlet with Specified Exit Aerodynamic Parameters -- Inverse Design of Curved Shock Wave Compression Surface on Basis of Specified Wall Aerodynamic Parameters -- Inverse Design of Axisymmetric Reference Flow Field on Basis of Specified Wall Aerodynamic Parameters -- Inverse Design and Experiment of Hypersonic Curved Shock Wave Compression Inlet -- Concept of Hypersonic Adaptive Variable Geometric Curved Compression Inlet -- Features and Drag Reduction Analysis of Drag in Hypersonic Inlet -- The Development of Curved Compression and Application Prospect. |
| Record Nr. | UNISA-996418170303316 |
|
Zhang Kun-Yuan
|
||
| Singapore : , : Springer Singapore : , : Imprint : Springer, , 2020 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. di Salerno | ||
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