Aeronautics & Astronautics - Fluid Sciences > Aerodynamics: Page 6

No. 30001 Flow over nozzle: throat conditions in supersonic nozzle No. 30002 Flow over nozzle: throat conditions in supersonic diffuser No. 30003 Nozzle flow: throat and outlet No. 30004 Area-Mach number relation in nozzle flow No. 30005 Mach numbers over flow horizontal path in nozzle flow No. 30006 Pressure-temperature ratios over flow horizontal path in nozzle flow No. 30007 Exit pressure in nozzle flow No. 30008 Mach numbers and pressure ratio over flow horizontal path in nozzle No. 30009 Differential mass versus exit pressure No. 30010 Mach number and pressure distribution in nozzle flow No. 30011 Shock waves in nozzle flow No. 30012 Upstream and downstream separation No. 30013 Long nozzle: normal shock wave at exit No. 30014 Long nozzle: Mach number distribution No. 30015 Long nozzle: pressure distribution No. 30016 Oblique shock wave at nozzle exit No. 30017 Convergent-divergent duct: finding shock wave No. 30018 Nozzle flow: shock wave between throat and exit No. 30019 Ideal isentropic diffuser No. 30020 Weak normal shock wave inside long diffuser No. 30021 Supersonic wind tunnel: configuration and object placement No. 30022 Outlet part of nozzle No. 30023 Oblique shock diffuser in wind tunnel No. 30024 Shock wave along airfoil: Euler and potential shocks No. 30045 Shock wave on supercritical airfoils No. 30046 Flow around small bump along with its shock waves No. 30047 Flow around small bump: constant potential along sloped lines No. 30048 Flow around thin airfoil at supersonic speed No. 30049 Pressure distribution of thin airfoil as function of mach number No. 30050 Supersonic airfoil: flat plate at small angle of attack No. 30051 Diamond shape airfoil: drag dependence on airfoil thickness No. 30052 Parabolic shape airfoil: drag dependence on airfoil thickness No. 30053 Superposition principle in drag analysis of airfoil No. 30054 Lift & drag distributions of parabolic airfoil at various mach numbers No. 30055 Plots of lift coefficient of diamond airfoil at several mach numbers No. 30056 Influence of thickness and camber in airfoil shape No. 30057 Superposition principle for lift distribution analysis of airfoil No. 30058 Pressures on airfoil with camber No. 30059 Lift coefficient of triangular airfoil No. 30060 Coordinate frame setup for flow analysis around airfoil No. 30061 Linearized supersonic flow analysis around diamond airfoil No. 30062 Linearized supersonic flow analysis around biconvex airfoil No. 30063 Flow over wall with sinusoidal shape No. 30064 Potential function of flow along sinusoidal surface No. 30065 Shock wave propagation along sinusoidal surface No. 30066 Unsteady wave motion: stationary normal shock wave No. 30067 Unsteady wave motion: moving normal shock wave No. 30068 Shock tube: configuration and pressure distribution No. 30069 Shock tube: wave propagation and pressure distribution No. 30070 Reflection of shock waves: incident shock
 

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