This book provides a comprehensive, practical treatment of aerodynamics of supersonic intakes in both civil and military types of aircraft. The problems of both internal and external airflow are investigated. Simple mathematics are used only in analysis, and emphasis is placed on giving a physical picture of the flow, often with the aid of illustrations. The new edition takes account of the increase in computer based solutions of intake flow fields and correlates experimental work with results from computer programs.
Les informations fournies dans la section « Synopsis » peuvent faire référence à une autre édition de ce titre.