نام کتاب: ایرودینامیک موشک

نویسنده: Jack N. Nielsen

مشخصات: Published by AIAA, © 1988, 450 pages / University Microfilms International Ann Arbor, Michigan USA

The "Bible" of missile aerodynamics

توضیحات: این کتاب از کتب مرجع معرفی شده توسط AIAA در رابطه با منابع آیرودینامیک کاربردی میباشد

The similarities between the airplane and the missile extend beyond their flying capabilities, and at higher operational speeds, the configuration distinctions become even less apparent. Missile Aerodynamics, a classic now available from AIAA and Nielsen Engineering and Research, Inc., combines the best of missile and airplane aerodynamics, drawing extensively from numerous technical papers to present a rational and unified account of the principles behind missile projection. Evaluate the missile versus the airplane in a multitude of areas, from longitudinal acceleration, wing loading, roll and dynamic stability, guidance and navigation, and more.

J.N. Nielsen covers every aspect of missile aerodynamics, from the classification of missiles and basic formulas to innovative aerodynamic controls. In one reliable reference, readers will find hundreds of schematics, equations, and tables with practical applications in missile design and engineering. Originally published by Nielsen Engineering and Research, Inc.

Table of Contents:

Introduction
Formulas Commonly Used in Missile Aerodynamics
Slender-Body Theory at Supersonic and Subsonic Speeds
Aerodynamics of Bodies
Vortices
Wing-Body Interference
Downwash, Sidewash, and the Wake
Wing-Tail Interference
Aerodynamic Controls
Drag
Stability Derivatives

نوشته شده در 86/12/19 توسط Admin | لينك ثابت | ثبت سفارش |