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The book investigates the complex phenomenon of unsteady transonic flow, a critical area in aerodynamics. Landahl, a recognized authority in the field, draws upon extensive research and theoretical frameworks to analyze the behavior of airflow at speeds approaching the speed of sound. The work focuses on the mathematical models and physical principles governing these flows, particularly the shock wave dynamics and their impact on aircraft performance. It aims to provide a comprehensive understanding of the challenges and intricacies involved in designing aircraft that operate efficiently in this flight regime.
The subject matter points to a dense, specialist text aimed at advanced students and researchers in aerospace engineering and fluid dynamics. The focus on unsteady transonic flow suggests a deep dive into complex theoretical and computational aspects of aerodynamics. The author's presumed expertise indicates a rigorous and authoritative treatment of the material, likely serving as a valuable reference for those working in high-speed flight research and design.
Page Count:
134
Publication Date:
1989-01-01
ISBN-10:
0521356644
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