Written to teach students the nature of transonic flow and its
mathematical foundation, this book offers a much-needed introduction to
transonic aerodynamics. The authors present a quantitative and
qualitative assessment of subsonic, supersonic and transonic flow around
bodies in two and three dimensions. The book reviews the governing
equations and explores their applications and limitations as employed in
modeling and computational fluid dynamics.
Some concepts, such as shock and expansion theory, are examined from a
numerical perspective. Others, including shock-boundary-layer
interaction, are discussed from a qualitative point of view. The book
includes 60 examples and more than 200 practice problems. The authors
also offer analytical methods such as Method of Characteristics (MOC)
that allow readers to practice with the subject matter.
The result is a wealth of insight into transonic flow phenomena and
their impact on aircraft design, including compressibility effects,
shock and expansion waves, shock-boundary-layer interaction and
aeroelasticity.