机读格式显示(MARC)

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• 003 SCNU

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• 008 890614s1990 nyua b 001 0 eng

• 010 __ |a 89012442

• 020 __ |a 0070016739

• 040 __ |a DLC |c DLC |d CPO |d FDU

• 050 00 |a QA911 |b .A6 1990

• 082 00 |a 629.132/323 |2 20

• 093 __ |a V211.1 |2 4

• 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.

• 250 __ |a 2nd ed.

• 260 __ |a New York : |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).

• 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.

• 650 _0 |a Gas dynamics.

• 920 __ |a 231010 |z 2

• 920 __ |a 212020 |z 2

• 920 __ |a 242020 |z 2

• 920 __ |a 262070 |z 1

• 950 __ |a SCNU |f V211.1/A547

• 998 __ |a FDU

• 999 __ |t C |A hwei2 |a 20040510 15:32:58 |M zxq |m 20040524 10:53:07 |G zxq |g 20040524 10:53:10

• 000 1000002592

• 991 __ |a 022004001158

• 907 __ |a SCNU |f V211.1/A547