Cargando…
Active Spanwise Lift Control
Active Spanwise Lift Control presents a novel approach to tackle the gust alleviation problem. Traditional approaches typically attempt to suppress the structural response at discrete points of the wing using only the conventional control surfaces (aileron, elevator, rudder), resulting in limited co...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Otros Autores: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Reston :
American Institute of Aeronautics & Astronautics,
2020.
|
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
| LEADER | 00000cam a2200000Mu 4500 | ||
|---|---|---|---|
| 001 | EBOOKCENTRAL_on1321788345 | ||
| 003 | OCoLC | ||
| 005 | 20240329122006.0 | ||
| 006 | m o d | ||
| 007 | cr ||||||||||| | ||
| 008 | 220528s2020 xx o ||| 0 eng d | ||
| 040 | |a EBLCP |b eng |c EBLCP |d REDDC |d OCLCF |d OCLCO |d OCLCQ |d OCLCL | ||
| 020 | |a 9781624106309 | ||
| 020 | |a 1624106307 | ||
| 035 | |a (OCoLC)1321788345 | ||
| 050 | 4 | |a TL574.L5 |b .D537 2020 | |
| 082 | 0 | 4 | |a 629.13233 |2 23 |
| 049 | |a UAMI | ||
| 100 | 1 | |a Dias, Joaquim Neto. | |
| 245 | 1 | 0 | |a Active Spanwise Lift Control |h [electronic resource]. |
| 260 | |a Reston : |b American Institute of Aeronautics & Astronautics, |c 2020. | ||
| 300 | |a 1 online resource (205 p.) | ||
| 500 | |a Description based upon print version of record. | ||
| 505 | 0 | |a Cover -- Half Title -- Title Page -- Copyright Page -- Contents -- Preface -- List of Tables -- List of Figures -- Acknowledgements -- Chapter 1: Introduction -- 1.1 Motivation: The Quest for Increasingly Efficient Aircraft -- 1.2 Literature Review on Active Load Alleviation -- 1.3 Proposed Approach -- 1.4 Fundamental assumptions -- 1.5 Unique features of this book -- 1.6 Book Organization -- Chapter 2: Unsteady Aerodynamic Modeling of a Multiflap Wing -- 2.1 Quasi-Steady Aerodynamic Model -- 2.2 Unsteady Lifting-Line Theory (ULLT) -- 2.3 Unsteady Vortex Lattice Method (UVLM) | |
| 505 | 8 | |a 2.4 Verification of Aerodynamic Models -- 2.5 Assumptions and Constraints -- Chapter 3: Review of Model Order Reduction Methods -- 3.1 Introduction -- 3.2 Proper Orthogonal Decomposition: Fundamentals -- 3.3 Balanced Proper Orthogonal Decomposition -- 3.4 Eigensystem Realization Algorithm (ERA) -- 3.5 Example: Application to a Finite Element Model of a Cantilever Beam -- 3.6 Chapter Summary -- Chapter 4: Modal Identification of Aerodynamic Systems -- 4.1 Modal Identification from UVLM -- 4.2 Limits in Identifiability -- 4.3 Modal Identification from ULLT | |
| 505 | 8 | |a 4.4 Physical Interpretation of Aerodynamic Modes -- 4.5 Effects of Varying Wing Planform on the Mode Shapes and Eigenvalues -- 4.6 Chapter Summary -- Chapter 5: Spatial Control of Spanwise Lift Distribution -- 5.1 Model Output Expansion into Mode Shapes -- 5.2 Threshold for Model Truncation -- 5.3 Spatial-Temporal Controller Synthesis -- 5.4 Shape Control Problem -- 5.5 Gust Load Alleviation Problem -- 5.6 Gust Load Alleviation Problem with Gust Estimation -- 5.7 Chapter Summary -- 5.8 Future Developments of This Methodology -- Appendix A -- References -- Index -- Supporting Materials | |
| 520 | |a Active Spanwise Lift Control presents a novel approach to tackle the gust alleviation problem. Traditional approaches typically attempt to suppress the structural response at discrete points of the wing using only the conventional control surfaces (aileron, elevator, rudder), resulting in limited control authority, high-bandwidth actuator requirements, and necessity of gust field measurements ahead of the aircraft. In this book, the authors directly address th. | ||
| 590 | |a ProQuest Ebook Central |b Ebook Central Academic Complete | ||
| 650 | 0 | |a Gust loads. | |
| 650 | 0 | |a Lift (Aerodynamics) | |
| 650 | 0 | |a Trailing edge flaps. | |
| 650 | 0 | |a Airplanes |x Wings. | |
| 650 | 6 | |a Portance. | |
| 650 | 6 | |a Avions |x Ailes. | |
| 650 | 7 | |a Airplanes |x Wings |2 fast | |
| 650 | 7 | |a Gust loads |2 fast | |
| 650 | 7 | |a Lift (Aerodynamics) |2 fast | |
| 650 | 7 | |a Trailing edge flaps |2 fast | |
| 700 | 1 | |a Hubbard, James E. | |
| 758 | |i has work: |a Active spanwise lift control (Text) |1 https://id.oclc.org/worldcat/entity/E39PCH8PK8BHtrW6fktPGDG6Td |4 https://id.oclc.org/worldcat/ontology/hasWork | ||
| 776 | 0 | 8 | |i Print version: |a Dias, Joaquim Neto |t Active Spanwise Lift Control: a Distributed Parameter Approach |d Reston : American Institute of Aeronautics & Astronautics,c2020 |z 9781624105999 |
| 856 | 4 | 0 | |u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=29275813 |z Texto completo |
| 938 | |a ProQuest Ebook Central |b EBLB |n EBL29275813 | ||
| 994 | |a 92 |b IZTAP | ||