Performance, stability, dynamics, and control of airplanes / Bandu N. Pamadi.
By: Pamadi, Bandu N
Language: İngilizce Series: AIAA education seriesPublisher: Reston, VA : American Institute of Aeronautics and Astronautics, c2004Edition: 2nd edDescription: xix, 780 p. : ill. ; 24 cmISBN: 1563475839 (alk. paper)Subject(s): Hava dinamiği | Aerodynamics | Airplanes -- Control systems | Uçaklar -- Kontrol sistemleri | Airplanes -- Performance | Uçaklar -- Performans | Stability of airplanes | Kararlılık, UçaklardaLOC classification: TL671.4 | .P28 2004Online resources: Table of contents
Contents:
Review of Basic Aerodynamic Principles -- Aircraft Performance -- Static Stability and Control -- Equations of Motion and Estimation of Stability Derivatives -- Linear Systems, Theory, and Design: A Brief Review -- Airplane Response and Closed-Loop -- Inertia Coupling and Spin -- Stability and Control Problems at High Angles of Attack.
| Item type | Current location | Home library | Collection | Call number | Vol info | Copy number | Status | Date due | Barcode |
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Book
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Merkez Kütüphane Genel Koleksiyon / Main Collection | Merkez Kütüphane | Genel Koleksiyon | TL671.4 .P28 2004 (Browse shelf) | 1 | 1 | Available | 0014778 |
Browsing Merkez Kütüphane Shelves , Shelving location: Genel Koleksiyon / Main Collection , Collection code: Genel Koleksiyon Close shelf browser
| TL671.4 .A54 1999 Aircraft performance & design. | TL671.4 .A87 1997 An introduction to aircraft performance / | TL671.4 .E84 2000 Aircraft performance : | TL671.4 .P28 2004 Performance, stability, dynamics, and control of airplanes / | TL671.4 .S62 2001 Flight vehicle performance and aerodynamic control / | TL671.4 .Y43 2003 Introduction to aircraft flight mechanics : performance, static stability, dynamic stability, and classical feedback control / | TL672 .A2 1959 Theory of wing sections : including a summary of airfoil data / |
Review of Basic Aerodynamic Principles -- Aircraft Performance -- Static Stability and Control -- Equations of Motion and Estimation of Stability Derivatives -- Linear Systems, Theory, and Design: A Brief Review -- Airplane Response and Closed-Loop -- Inertia Coupling and Spin -- Stability and Control Problems at High Angles of Attack.
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