| 902 Harga | |
| 001 Hak Akses (open/membership) | membership |
| 700 Entri Tambahan Nama Orang | |
| 336 Content Type | text (rdacontent) |
| 264b Nama Penerbit | Springer Cham |
| 049 No. Barkod | 20-23-48707934 |
| 110 Entri Utama Badan Korporasi | |
| 338 Carrier Type | online resource (rdacarrier) |
| 490 Seri | Springer Aerospace Technology |
| 903 Stock Opname | |
| 053 No. Induk | 20-23-48707934 |
| 653 Kata Kunci | Aircraft conceptual design; control power assessment; sizing control effectors; trimmed aerodynamics; safety verification |
| 040 Sumber Pengatalogan | LibUI eng rda |
| 245 Judul Utama | Stability and Control of Conventional and Unconventional Aerospace Vehicle Configurations: A Generic Approach from Subsonic to Hypersonic Speeds |
| 592 Sumber Koleksi | Springerlink |
| 264c Tahun Terbit | 2019 |
| 650 Subyek Topik | Aerospace engineering; Aircraft; Aerodynamics--Design and construction. |
| 904c Penginput Data Pengadaan | |
| 904b Pemeriksa Lembar Kerja | Henny-Mei2024 |
| 520 Ringkasan/Abstrak/Intisari | This book introduces a stability and control methodology named AeroMech, capable of sizing the primary control effectors of fixed wing subsonic to hypersonic designs of conventional and unconventional configuration layout. Control power demands are harmonized with static-, dynamic-, and maneuver stability requirements, while taking the six-degree-of-freedom trim state into account. The stability and control analysis solves the static- and dynamic equations of motion combined with non-linear vortex lattice aerodynamics for analysis.
The true complexity of addressing subsonic to hypersonic vehicle stability and control during the conceptual design phase is hidden in the objective to develop a generic (vehicle configuration independent) methodology concept. The inclusion of geometrically asymmetric aircraft layouts, in addition to the reasonably well-known symmetric aircraft types, contributes significantly to the overall technical complexity and level of abstraction. The first three chapters describe the preparatory work invested along with the research strategy devised, thereby placing strong emphasis on systematic and thorough knowledge utilization. The engineering-scientific method itself is derived throughout the second half of the book.
This book offers a unique aerospace vehicle configuration independent (generic) methodology and mathematical algorithm. The approach satisfies the initial technical quest: How to develop a ?configuration stability & control? methodology module for an advanced multi-disciplinary aerospace vehicle design synthesis environment that permits consistent aerospace vehicle design evaluations? |
| 536 Catatan Informasi Pendanaan | BPPTN 2019 |
| 900 Tanggal Pembelian | 08/05/2024 |
| 020 ISBN (R) | 9783030168568 |
| 090 No. Panggil Setempat | e20511006 |
| 245c Pertanggungjawaban | |
| 337 Media Type | computer (rdamedia) |
| 340 Bentuk Medium | pdf |
| 100 Entri Utama Nama Orang | Chudoba, Bernd, author |
| 250 Edisi | |
| 264a Kota Terbit | Switzerland |
| 300 Deskripsi Fisik | xxxiv, 392 pages |
| 904a Pengisi Lembar Kerja | Kayla |
| 856 Akses dan Lokasi Elektronik | http://link.springer.com/openurl?genre=book&isbn=978-3-030-16856-8 |
| 041 Kode Bahasa | eng |