TY  - BOOK
T1  - High-Speed Aerodynamics
T2  - Prentice-Hall Aeronautical Engineering Series
A1  - Sibert, Harold W.
LA  - English
PP  - New York
PB  - Prentice-Hall
YR  - 1948
UL  - https://catalogo.bibliotecas.unlp.edu.ar/Record/dfi.9734
AB  - 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.
OP  - 280
KW  - ENERGIA
KW  - TERMODINAMICA
KW  - VELOCIDAD DEL SONIDO
KW  - NUMERO DE MACH
KW  - ATMOSFERA STANDAR
KW  - FLUJO EN TUNEL
KW  - FLUJO COMPRESIBLE
KW  - FLUJO POTENCIAL
KW  - FLUJO SUPERSONICO
KW  - ONDA DE CHOQUE
KW  - ALTIMETRO
KW  - VELOCIMETRO
KW  - BERNOULLI
KW  - EULER
ER  -