عرض عادي
Performance, stability, dynamics, and control of airplanes / Bandu N. Pamadi.
نوع المادة :
نصالسلاسل:AIAA education seriesالناشر:Reston, VA : American Institute of Aeronautics and Astronautics, c2004. 2004الطبعات:2nd edوصف:xix, 780 pages : illustrations ; 24 cmنوع المحتوى:- text
- unmediated
- volume
- 1563475839 (HBK)
- TL671.4 P28 2004
المحتويات:
Review of Basic Aerodynamic Principles -- Aircraft Performance -- StaticStability and Control -- Equations of Motion and Estimation of Stability Derivatives -- Linear Systems, Theory, and Design: A Brief Review -- Airplane Responseand Closed-Loop -- Inertia Coupling and Spin -- Stability and Control Problems at High Angles of Attack.
| نوع المادة | المكتبة الحالية | رقم الطلب | رقم النسخة | حالة | تاريخ الإستحقاق | الباركود | |
|---|---|---|---|---|---|---|---|
كتاب
|
UAE Federation Library | مكتبة اتحاد الإمارات General Collection | المجموعات العامة | TL671.4 P28 2004 (إستعراض الرف(يفتح أدناه)) | C.1 | Library Use Only | داخل المكتبة فقط | 30010000247172 | ||
|
كتاب
|
UAE Federation Library | مكتبة اتحاد الإمارات General Collection | المجموعات العامة | TL671.4 P28 2004 (إستعراض الرف(يفتح أدناه)) | C.2 | المتاح | 30010000247163 |
Browsing UAE Federation Library | مكتبة اتحاد الإمارات shelves, Shelving location: General Collection | المجموعات العامة إغلاق مستعرض الرف(يخفي مستعرض الرف)
| TL671.3 B56 1997 Biplane to monoplane : aircraft development 1919-39 / | TL671.4 G52 1997 The definition, understanding and design of aircraft handling qualities / | TL671.4 P28 2004 Performance, stability, dynamics, and control of airplanes / | TL671.4 P28 2004 Performance, stability, dynamics, and control of airplanes / | TL671.6 C88 1999 Understanding aircraft structures / | TL671.6 .L3 2010 Aircraft structures / | TL671.6 .M36 2013 Aircraft structures for engineering students / |
Review of Basic Aerodynamic Principles -- Aircraft Performance -- StaticStability and Control -- Equations of Motion and Estimation of Stability Derivatives -- Linear Systems, Theory, and Design: A Brief Review -- Airplane Responseand Closed-Loop -- Inertia Coupling and Spin -- Stability and Control Problems at High Angles of Attack.
