Simulation of flight test conditions in the langley pilot transonic cryogenic tunnel [NASA TN D 7811-7820
/ Kilgore, Robert A. [...et al.]
.- Washington: NASA, 1974
.- various pagings.
.- ( National Aeronautics and Space Administration, NASA Technical Report
Subject Headings:
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;
Copy Details:
Acc. No.: TR002549 [TN D7811-D, Full Call No.: , Item type: Technical Report , Location: COMPACT STORAGE (BASEMENT),
------------------------- --------------------- ------ --------- ------- ------- --------- --------
Subject Headings:
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;
Copy Details:
Acc. No.: TR002549 [TN D7811-D, Full Call No.: , Item type: Technical Report , Location: COMPACT STORAGE (BASEMENT),
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