| LDR | | 00000cam u2200205 a 4500 |
| 001 | | 000013619125 |
| 005 | | 20151012104946 |
| 008 | | 151001s2011 nyua b 001 0 eng d |
| 020 | |
▼a 0073398101 :
▼c $292.33 |
| 020 | |
▼a 9780073398105 |
| 035 | |
▼a (KERIS)BIB000012412196 |
| 040 | |
▼a 241018
▼c 241018
▼d 224010 |
| 050 | 00 |
▼a TL570
▼b .A677 2011 |
| 082 | 04 |
▼a 629.1323
▼2 22 |
| 090 | |
▼a 629.1323
▼b A54fm5 |
| 100 | 1 |
▼a Anderson, John David. |
| 245 | 10 |
▼a Fundamentals of aerodynamics /
▼c John D. Anderson, Jr. |
| 250 | |
▼a 5th ed. |
| 260 | |
▼a New York :
▼b McGraw-Hill,
▼c c2011. |
| 300 | |
▼a xxiii, 1106 p. :
▼b ill. ;
▼c 24 cm. |
| 490 | 1 |
▼a Anderson series |
| 490 | 1 |
▼a McGraw-Hill series in aeronautical and aerospace engineering |
| 504 | |
▼a Includes bibliographical references and index. |
| 505 | 0 |
▼a Aerodynamics -- Aerodynamics -- Fundamentals of inviscid, incompressible flow -- Incompressible flow over airfoils -- Incompressible flow over finite wings -- Three-dimensional incompressible flow -- Compressible flow -- Normal shock waves and related topics -- Oblique shock and expansion waves -- Compressible flow through nozzles, diffusers, and wind tunnels -- Subsonic compressible flow over airfoils -- Linearized supersonic flow -- Introduction to numerical techniques for nonlinear supersonic flow -- Elements of hypersonic flow -- Introduction to the fundamental principles and equations of viscous flow -- Special case. |
| 650 | 0 |
▼a Aerodynamics. |
| 800 | 1 |
▼a Anderson, John David.
▼t Anderson series. |
| 830 | 0 |
▼a McGraw-Hill series in aeronautical and aerospace engineering. |