Introduction to Aerodynamics of a Compressible Fluid |
Contents
PART I | 1 |
CHAPTER PAGE 1 BASIC THERMODYNAMICS | 3 |
EQUATIONS OF MOTION IN ONE DIMENSION | 13 |
Copyright | |
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Common terms and phrases
airfoil approximation becomes boundary condition boundary layer channel Chapter characteristic compressible fluid computed constant continuity equation corresponding curve deflection angle density gradient diagram differential equation dx₁ energy equation entropy equa equations of motion expansion wave finite flow deflection flow field free stream friction function Hence hodograph equations hodograph plane incompressible flow integral isentropic flow knife edge limiting line M₁ Mach number Mach wave mass flow method momentum normal shock normal shock wave nozzle oblique shock oblique shock wave obtain one-dimensional P₁ parallel parameters perturbation physical plane pitot tube pressure coefficient problem ratio relation reservoir pressure satisfied shock wave small-perturbation solution speed of sound stream tube streamline subsonic subsonic flow supersonic flow surface temperature test section theory thickness throat tion transformation u₁ wall wind tunnel zero ρο ӘФ др Ро მა