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|n Title subscribed to via ProQuest Academic Complete
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| 050 |
|
4 |
|a TL671.2
|b .N5 2010eb
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| 082 |
0 |
4 |
|a 629.134/1
|2 22
|
| 049 |
|
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|a UAMI
|
| 100 |
1 |
|
|a Nicolai, Leland M.
|q (Leland Malcolm)
|1 https://id.oclc.org/worldcat/entity/E39PCjFkmBcrx9DHHVvhTV3YT3
|
| 245 |
1 |
0 |
|a Fundamentals of aircraft and airship design.
|n Volume 1,
|p Aircraft design /
|c Leland M. Nicolai, Grant E. Carichner.
|
| 260 |
|
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|a Reston, Va. :
|b American Institute of Aeronautics and Astronautics,
|c 2010.
|
| 300 |
|
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|a 1 online resource (xxii, 883 pages, 24 unnumbered pages of plates) :
|b illustrations (some color)
|
| 336 |
|
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|a text
|b txt
|2 rdacontent
|
| 337 |
|
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|a computer
|b c
|2 rdamedia
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| 338 |
|
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|a online resource
|b cr
|2 rdacarrier
|
| 347 |
|
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|a data file
|
| 490 |
1 |
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|a AIAA educational series
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| 500 |
|
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|a Rev. and expanded ed. of: Fundamentals of aircraft design / Leland M. Nicolai. 1975.
|
| 504 |
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|a Includes bibliographical references and index.
|
| 505 |
0 |
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|a COVER -- TITLE -- COPYRIGHT -- FOREWORD -- CONTENTS -- LIST OF COLOR PLATES -- PREFACE -- Chapter 1: Introduction -- Chapter 2: Review of Practical Aerodynamics -- Chapter 3: Aircraft Performance Methods -- Chapter 4: Aircraft Operating Envelope -- Chapter 5: Preliminary Estimate of Takeoff Weight -- Chapter 6: Estimating the Takeoff Wing Loading -- Chapter 7: Selecting the Planform and Airfoil Section -- Chapter 8: Preliminary Fuselage Sizing and Design -- Chapter 9: High-Lift Devices -- Chapter 10: Takeoff and Landing Analysis
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| 505 |
8 |
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|a Chapter 11: Preliminary Sizing of the Vertical and Horizontal TailsChapter 12: Designing for Survivability (Stealth) -- Chapter 13: Estimating Wing�Body Aerodynamics -- Chapter 14: Propulsion System Fundamentals -- Chapter 15: Turbine Engine Inlet Design -- Chapter 16: Corrections forTurbine Engine Installation -- Chapter 17: Propeller Propulsion Systems -- Chapter 18: Propulsion System Thrust Sizing -- Chapter 19: Structures and Materials -- Chapter 20: Refined Weight Estimate -- Chapter 21 Static Stability and Control
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| 505 |
8 |
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|a Chapter 22: Trim Drag and Maneuvering FlightChapter 23: Control Surface Sizing Criteria -- Chapter 24: Life Cycle Cost -- Chapter 25: Trade Studies and Sizing -- Appendix A: Conversions -- Appendix B: Atmospheric Data -- Appendix C: Isentropic Compressible Flow Functions -- Appendix D: Normal Shock Functions for a Perfect Gas -- Appendix E: Plane Oblique and Conical Shocks -- Appendix F: NACA Airfoil Nomenclature and Data -- Appendix G: Aerodynamic Data of Real Aircraft -- Appendix H: Aerodynamics of Wing�Body Combinations -- Appendix I: Aircraft Weights Data
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| 505 |
8 |
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|a Appendix J: Propulsion DataAppendix K: Miscellaneous Data -- INDEX -- SUPPORTING MATERIALS
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| 546 |
|
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|a English.
|
| 590 |
|
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|a ProQuest Ebook Central
|b Ebook Central Academic Complete
|
| 590 |
|
|
|a Knovel
|b ACADEMIC - Aerospace & Radar Technology
|
| 650 |
|
0 |
|a Airplanes
|x Design and construction
|x History.
|
| 650 |
|
0 |
|a Airships
|x Design and construction
|x History.
|
| 650 |
|
0 |
|a Aeronautics
|v Pictorial works.
|
| 650 |
|
6 |
|a Avions
|x Conception et construction
|x Histoire.
|
| 650 |
|
7 |
|a Aeronautics
|2 fast
|
| 650 |
|
7 |
|a Airplanes
|x Design and construction
|2 fast
|
| 650 |
|
7 |
|a Airships
|x Design and construction
|2 fast
|
| 655 |
|
7 |
|a History
|2 fast
|
| 655 |
|
7 |
|a Pictorial works
|2 fast
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| 700 |
1 |
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|a Carichner, Grant.
|
| 700 |
1 |
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|a Nicolai, Leland M.
|q (Leland Malcolm).
|t Fundamentals of aircraft design.
|
| 758 |
|
|
|i has work:
|a Volume 2 Fundamentals of aircraft and airship design Aircraft design and case studies (Text)
|1 https://id.oclc.org/worldcat/entity/E39PCFV7BVCVHWcWJPRPKKHwG3
|4 https://id.oclc.org/worldcat/ontology/hasWork
|
| 776 |
0 |
8 |
|i Print version:
|a Nicolai, Leland M. (Leland Malcolm).
|t Fundamentals of aircraft and airship design.
|d Reston, Va. : American Institute of Aeronautics and Astronautics, 2010
|w (DLC) 2010012955
|
| 830 |
|
0 |
|a AIAA educational series.
|
| 856 |
4 |
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|u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=3111641
|z Texto completo
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