Sibert, Harold W. <br/><br/>
High-Speed Aerodynamics /   
Harold W. Sibert. 
 - New York :   Prentice-Hall,   1948. 
 - 280 p. 
 - Prentice-Hall Aeronautical Engineering Series .
<br/><br/> 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. 
<br/><br/><label>Subjects--Topical Terms: </label><br/>ENERGIA<br/>TERMODINAMICA<br/>VELOCIDAD DEL SONIDO<br/>NUMERO DE MACH<br/>ATMOSFERA STANDAR<br/>FLUJO EN TUNEL<br/>FLUJO COMPRESIBLE<br/>FLUJO POTENCIAL<br/>FLUJO SUPERSONICO<br/>ONDA DE CHOQUE<br/>ALTIMETRO<br/>VELOCIMETRO<br/>VELOCIMETRO<br/>BERNOULLI<br/>EULER
<br/><br/><label>Universal Decimal Class. No.: </label>531.33-255