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نمایش مورد 1-10 از 42 نتیجه جستجو شده.
عملیات
NACA-TN-2335 : A plan-form parameter for correlating certain aerodynamic characteristics of swept wings
سازمان:
NASA - National Aeronautics and Space Administration (NASA)
زبان:
English
سال:
1951
قیمت: 55000 تومان
NACA-TN-1711 : Approximate relations for hinge-moment parameters of control surfaces on swept wings at low Mach numbers
سازمان:
NASA - National Aeronautics and Space Administration (NASA)
زبان:
English
سال:
1948
قیمت: 55000 تومان
NACA-TN-2229 : The effect of end plates on swept wings at low speed
سازمان:
NASA - National Aeronautics and Space Administration (NASA)
زبان:
English
سال:
1950
قیمت: 55000 تومان
NACA-TN-1977 : Summary of the theoretical lift, damping-in-roll, and center-of-pressure characteristics of various wing plan forms at supersonic speeds
سازمان:
NASA - National Aeronautics and Space Administration (NASA)
زبان:
English
سال:
1949
قیمت: 55000 تومان
NASA-TN-D-7099 : Effect of wing design on the longitudinal aerodynamic characteristics of a wing-body model at subsonic speeds
سازمان:
NASA - National Aeronautics and Space Administration (NASA)
زبان:
English
سال:
1972
قیمت: 55000 تومان
NASA-TN-D-1394 : A tabulation of wind-tunnel pressure data and section aerodynamic characteristics at mach numbers of 1.61 and 2.01 for two trapezoidal and three delta wings having different surface shapes
سازمان:
NASA - National Aeronautics and Space Administration (NASA)
زبان:
English
سال:
1962
قیمت: 55000 تومان
NACA-TN-2294 : Lift and pitching derivatives of thin sweptback tapered wings with streamwise tips and subsonic leading edges at supersonic speeds
سازمان:
NASA - National Aeronautics and Space Administration (NASA)
زبان:
English
سال:
1951
قیمت: 55000 تومان
NACA-TN-2146 : On the effect of subsonic trailing edges on damping in roll and pitch of thin sweptback wings in a supersonic stream
سازمان:
NASA - National Aeronautics and Space Administration (NASA)
زبان:
English
سال:
1950
قیمت: 55000 تومان
NACA-TN-1581 : Approximate relations and charts for low-speed stability derivatives of swept wings
سازمان:
NASA - National Aeronautics and Space Administration (NASA)
زبان:
English
سال:
1948
قیمت: 55000 تومان
NACA-TN-2114 : Theoretical lift and damping in roll of thin wings with arbitrary sweep and taper at supersonic speeds: supersonic leading and trailing edges
سازمان:
NASA - National Aeronautics and Space Administration (NASA)
زبان:
English
سال:
1950
قیمت: 55000 تومان