机读格式显示(MARC)
- 000 01441cam 2200301 a 4500
- 008 040831s1990 maua b 001 0 eng
- 040 __ |a DLC |c DLC |d CPO |d FDU
- 082 00 |a 629.132/323 |2 20
- 099 __ |a CAL 022001107203
- 100 1_ |a Anderson, John David.
- 245 10 |a Modern compressible flow : |b with historical perspective / |c John D. Anderson, Jr.
- 260 __ |a Boston : |b McGraw-Hill, |c c1990.
- 300 __ |a xix, 650 p. : |b ill. ; |c 25 cm.
- 440 _0 |a McGraw-Hill series in aeronautical and aerospace engineering
- 504 __ |a Includes bibliographical references (p. 639-644) and index.
- 505 0_ |a Compressible flow -- Integral forms of the conservation equations for inviscid flows -- One-dimensional flow -- Oblique shock and expansion waves -- Quasi-one-dimensional flow -- Differential conservation equations for inviscid flows -- Unsteady wave motion -- General conservation equations revisited -- Linearized flow -- Conical flow -- Numerical techniques for steady supersonic flow -- Time-marching technique -- Three-dimensional flow -- Transonic flow -- Hypersonic flow -- Properties of high-temperature gases -- High-temperature flows.
- 650 _0 |a Fluid dynamics.
- 950 __ |a JHUL |b O35 |c A547=2