A comprehensive development history of missile airframe aerodynamics is presented, encompassing ground-, ground vehicle-, ship-, and air-launched categories of all ranges short of strategic. Emphasis is placed on the swift acceleration of missile configuration aerodynamics by German researchers in the course of the Second World War and by U.S. research establishments thereafter, often on the foundations laid by German workers. Examples are given of foundational airframe design criteria established by systematic researches undertaken in the 1950s, regarding L/D ratios, normal force and pitching moment characteristics, minimum drag forebodies and afterbodies, and canard and delta winged configuration aerodynamics.
Historical review of tactical missile airframe developments
1992-01-01
Sonstige
Keine Angabe
Englisch
Navy Tactical Missile Propulsion Market Developments
British Library Conference Proceedings | 1995
|Historical review of missile aerodynamic developments
NTRS | 1989
|Historical Review of Missile Aerodynamic Developments
NTIS | 1989
|Historical review of missile aerodynamic developments
NTRS | 1989
|