High-Speed Aerodynamics / Harold W. Sibert.
Tipo de material:
TextoSeries Prentice-Hall Aeronautical Engineering SeriesDetalles de publicación: New York : Prentice-Hall, 1948.Descripción: 280 pTema(s): Alcance y contenido: 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.
Libro
| Biblioteca actual | Signatura topográfica | Estado | Fecha de vencimiento | Código de barras | |
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| Koha Ingenieria | 531.33-255 SIB Bloque 7 (Navegar estantería(Abre debajo)) | Disponible | A0306 |
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| 531.3-324 HAT Bloque 7 The viscosity of liquids | 531.3-324 TEL-Bloque 7 Unsteady viscous flows. | 531.3-324 VIL Bloque 7 Lecons sur les Fluides Visqueux | 531.33-255 SIB Bloque 7 High-Speed Aerodynamics / | 531.3-33RIC-Bloque 7 Dynamics of real Fluids | 531.33:519.6 BLA Bloque 9 Computational fluid dynamics : principles and applications / | 531.33:519.6 BRI Bloque 7 Introducción al modelado numérico de flujos reactivos / |
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.
Ubic.:531.33-255 SIB Ej.1 PRES
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