Simulation of flight test conditions in the langley pilot transonic cryogenic tunnel [NASA TN D 7811-7820
By: NASA : National Aeronautics and Space Administration.
Material type:
BookSeries: National Aeronautics and Space Administration, NASA Technical Report. Publisher: Washington NASA 1974Description: various pagings.Subject(s): NASA Technical Report -- National Aeronautics and Space Administration -- TR002550 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; -- TR002551 NASA TN D-7813 : Calculation of the twist distribution of wings designed for cruise at transonic speeds; -- TR002552 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; -- TR002553 NASA TN D-7815 : Experimental investigation of the cornering characteristics of 18*5.5, type VII, aircraft tires with different tread patterns; -- TR002554 NASA TN D-7816 : Static tests of a simulated upper surface blown jet-flap configuration utilizing a full-size turbofan engine; -- TR002555 NASA TN D-7817 : Effects of nozzle interfairing modifications on longitudinal aerodynamic characteristics of a twin-jet, variable-wing-sweep fighter model; -- TR002556 NASA TN D-7818 : Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades; -- TR002557 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; -- TR002558 NASA TN D-7820 : Digital program for solving the linear stochastic optimal control and estimation problem| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
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PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | Not for loan | TR002549 [TN D7811-D |
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;
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;
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