| 000 | 03278nam a22001817a 4500 | ||
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| 005 | 20200219112202.0 | ||
| 008 | 200219b xxu||||| |||| 00| 0 eng d | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 110 | _aNASA : National Aeronautics and Space Administration | ||
| 245 |
_aSimulation of flight test conditions in the langley pilot transonic cryogenic tunnel [NASA TN D 7811-7820 _cKilgore, Robert A. [...et al.] |
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| 260 |
_aWashington _bNASA _c1974 |
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| 300 | _avarious pagings | ||
| 440 | _aNational Aeronautics and Space Administration, NASA Technical Report | ||
| 505 | _aNASA TN D-7812 : Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities; NASA TN D-7813 : Calculation of the twist distribution of wings designed for cruise at transonic speeds; NASA TN D-7814 : The effect of canard leading-edge sweep and dihedral angle on the longitudinal and lateral aerodynamic characteristics of a close-coupled canard-wing configuration; NASA TN D-7815 : Experimental investigation of the cornering characteristics of 18*5.5, type VII, aircraft tires with different tread patterns; NASA TN D-7816 : Static tests of a simulated upper surface blown jet-flap configuration utilizing a full-size turbofan engine; NASA TN D-7817 : Effects of nozzle interfairing modifications on longitudinal aerodynamic characteristics of a twin-jet, variable-wing-sweep fighter model; NASA TN D-7818 : Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades; NASA TN D-7819 : Flight-determined lag of angle-of-attack and angle-of-sideslip sensors in the YF-12A airplane from analysis of dynamic maneuvers; NASA TN D-7820 : Digital program for solving the linear stochastic optimal control and estimation problem; | ||
| 650 |
_aNASA Technical Report _xNational Aeronautics and Space Administration _xTR002550 NASA TN D-7812 : Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities; _xTR002551 NASA TN D-7813 : Calculation of the twist distribution of wings designed for cruise at transonic speeds; _xTR002552 NASA TN D-7814 : The effect of canard leading-edge sweep and dihedral angle on the longitudinal and lateral aerodynamic characteristics of a close-coupled canard-wing configuration; _xTR002553 NASA TN D-7815 : Experimental investigation of the cornering characteristics of 18*5.5, type VII, aircraft tires with different tread patterns; _xTR002554 NASA TN D-7816 : Static tests of a simulated upper surface blown jet-flap configuration utilizing a full-size turbofan engine; _xTR002555 NASA TN D-7817 : Effects of nozzle interfairing modifications on longitudinal aerodynamic characteristics of a twin-jet, variable-wing-sweep fighter model; _xTR002556 NASA TN D-7818 : Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades; _xTR002557 NASA TN D-7819 : Flight-determined lag of angle-of-attack and angle-of-sideslip sensors in the YF-12A airplane from analysis of dynamic maneuvers; _xTR002558 NASA TN D-7820 : Digital program for solving the linear stochastic optimal control and estimation problem; |
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| 942 | _cBK | ||
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_c561386 _d561386 |
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