High-Speed Aerodynamics /
Fundamental relations - Thermodynamical relations - Energy, Bernoulli, and Euler equations - Entropy and isentropic flow - Speed of sound - Mach number - Dynamic and impact pressures - Pressure coefficients - Critical conditions - Standard atmosphere - Altimeter, airspeed indicator, machmeter, and t...
Guardado en:
| Autor principal: | |
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| Formato: | Libro |
| Lenguaje: | Inglés |
| Publicado: |
New York :
Prentice-Hall,
1948.
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| Colección: | Prentice-Hall Aeronautical Engineering Series
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| Materias: | |
| Aporte de: | Registro referencial: Solicitar el recurso aquí |
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| 008 | 060510s1948 |||a fr||||| |0 0|eng d | ||
| 080 | |a 531.33-255 | ||
| 100 | 1 | |a Sibert, Harold W. |9 283916 | |
| 245 | 0 | 0 | |a High-Speed Aerodynamics / |c Harold W. Sibert. |
| 260 | |a New York : |b Prentice-Hall, |c 1948. | ||
| 300 | |a 280 p. | ||
| 490 | |a Prentice-Hall Aeronautical Engineering Series | ||
| 520 | 2 | |a Fundamental relations - Thermodynamical relations - Energy, Bernoulli, and Euler equations - Entropy and isentropic flow - Speed of sound - Mach number - Dynamic and impact pressures - Pressure coefficients - Critical conditions - Standard atmosphere - Altimeter, airspeed indicator, machmeter, and true airspeed meter - Determination of position error - True, indicated, calibrated, and equivalent airspeeds - Aerodynamic heating - Reversible adiabatic flow within a stream-tube - One-dimensional flow in a wind tunnel or nozzle - Partial-derivative equations for compressible flow - Disturbance potential - Ackeret supersonic theory - Flow through a shock wave - Normal shock wave - Supersonic flow past a wedge - Two-dimensional supersonic flow around a corner - Buseman parabolic formula - Supersonic flow past a cone - Adverse effects of high airplane mach numbers - Swept wings and wings of low aspect ratio - Determination of high-speed aerodynamic data - Wing drag from a wake survey - Tables and charts. | |
| 599 | |a Ubic.:531.33-255 SIB Ej.1 PRES | ||
| 650 | 4 | |a ENERGIA |9 263384 | |
| 650 | 4 | |a TERMODINAMICA |9 262699 | |
| 650 | 4 | |a VELOCIDAD DEL SONIDO |9 283917 | |
| 650 | 4 | |a NUMERO DE MACH |9 283918 | |
| 650 | 4 | |a ATMOSFERA STANDAR |9 281616 | |
| 650 | 4 | |a FLUJO EN TUNEL |9 283919 | |
| 650 | 4 | |a FLUJO COMPRESIBLE |9 274615 | |
| 650 | 4 | |a FLUJO POTENCIAL |9 274608 | |
| 650 | 4 | |a FLUJO SUPERSONICO |9 274742 | |
| 650 | 4 | |a ONDA DE CHOQUE |9 283687 | |
| 650 | 4 | |a ALTIMETRO |9 283920 | |
| 650 | 4 | |a VELOCIMETRO |9 278018 | |
| 650 | 4 | |a VELOCIMETRO |9 278018 | |
| 650 | 4 | |a BERNOULLI |9 283921 | |
| 650 | 4 | |a EULER |9 283922 | |
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