Aeronautics & Astronautics - Fluid Sciences > Aerodynamics: Page 5

No. 29942 Slender body of revolution at small angle of attack No. 29943 Perturbation velocity potential No. 29944 Flow source: mass balance in cross-flow plane No. 29945 Two dimensional flow past cylinder No. 29946 Distribution of doublets opposite to free stream flow No. 29947 Symmetric airfoil: nonexistence of vertical force with sharp end No. 29948 Cut-end symmetric airfoil: existence of vertical force No. 29949 Some pointed bodies: straight and curved body contours No. 29950 Side flow over finite wing No. 29951 Lifting lines for finite wing No. 29952 Pressure increment on infinitesimal decreasing volume body No. 29953 Subsonic flow over airfoil No. 29954 Transonic flow over airfoil: attached shock wave No. 29955 Supersonic flow over airfoils: various shock waves No. 29956 Hypersonic flow over conical body No. 29957 Added heat and work to control volume No. 29958 One-dimensional flow over symmetric body with constant area No. 29959 Two-dimensional flow over body with variable area No. 29960 Physical flow variables across control volume No. 29961 Physical flow variables across wave front No. 29962 Mach number behind shock wave versus Mach number in front of shock No. 29963 Ratio of densities before and after shock vs. Mach number prior shock No. 29964 Ratio of pressures before and after shock vs. Mach number prior shock No. 29965 Logarithmic plots of density ratio versus pressure ratio No. 29966 Plots of pressure vs. volume: isentropic and Hugoniot curves No. 29967 One-dimensional flow with heat addition No. 29968 Phase diagram describing chocked flow No. 29969 One dimensional flow with friction No. 29970 Investigation of flow variables at distinct points No. 29971 Fanno curve: h-s diagram No. 29972 Wave field induced by object moving at subsonic speed No. 29973 Wave field induced by object moving at supersonic speed No. 29974 Oblique shock on cone/wedge object No. 29975 Control volume around shock wave No. 29976 Shock wave angle versus deflection angle No. 29977 Flow and shock over wedge No. 29978 Flow and shock over cone No. 29979 Pressures around wedge under shock wave influence No. 29980 Shock polar No. 29981 Shock polar and contours of several Mach numbers No. 29982 Reflection of shock wave No. 29983 Left running shock wave No. 29984 Pressure distribution versus inclination angle No. 29985 Right running shock wave No. 29986 Pressure distributions versus inclination angle at two mach numbers No. 29987 Intersection of left-right running shock waves No. 29988 Shock wave creation in front of blunt body No. 29998 Control volume for nozzle flow analysis No. 29999 Convergent-divergent duck No. 30000 Expansive and compressive flows: exiting and entering flows
 

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