Rapid determination of near-optimum linear pitch programs for rocket boosters.
Linear segment pitch rate program for near optimum trajectory for rocket boosters
COMPUTER PROGRAM↗
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Determination of normal force and pitching moment characteristics of bodies of revolution at finite angles of attack - Extension of cross flow technique.
Drag coefficients used to evaluate normal force and pitching moment characteristics of revolving body at angle of attack
BLUNT BODY↗
Calculation of aerodynamic forces on a propeller in pitch or yaw
An analysis was made to determine the applicability of existing propeller theory and the theory of oscillating airfoils to the problem of determining the magnitude of the forces on propellers in pitch or yaw. Strip calculations using compressible airfoil characteristics were first made as though steady-state conditions existed successively at several blade positions of the propeller blades during one revolution. A theory of oscillating airfoils in pulsating incompressible potential flow was then considered from which it was possible to determine factors which would modify the steady-state forces.
PROPELLERS - PITCH AND YAW↗
MEASUREMENT OF PITCH DAMPING AT LARGE ANGLES OF OSCILLATION FOR PROPOSED MARS ATMOSPHERE-ENTRY VEHICLES
Pitch damping at large angles of oscillation for proposed mars atmosphere-entry vehicles - wind tunnel test methods
WIND TUNNEL↗
AERODYNAMIC CHARACTERISTICS IN PITCH AT A MACH NUMBER OF 2.01 OF SEVERAL WING-BODY COMBINATIONS WITH WEDGE-SHAPED BODIES LOCATED ABOVE AND BELOW A 54.5 DEG SWEPT DELTA WING
Aerodynamic characteristics in pitch of several wing-body combinations with wedge-shaped planform located above and below a swept delta wing
DELTA WING↗
THE INFLUENCE OF SHAPE ON AERODYNAMIC DAMPING OF OSCILLATORY MOTION DURING PLANET ATMOSPHERE ENTRY AND MEASUREMENT OF PITCH DAMPING AT LARGE OSCILLATION AMPLITUDES
Reentry vehicle shape effects on the accuracy and angle-of-attack amplitude and wind tunnel methods for measuring pitch damping
SPACECRAFT REENTRY↗
A Wind-Tunnel Investigation of the Effect of Changes in Base Contour on the Damping in Pitch of a Blunted Cone
Effect of changes in base contour on damping in pitch of blunted cone in wind tunnel
DAMPING↗
Effect of store pitch flexibility on flutter characteristics of a wing-store configuration at mach numbers near 0.85
Store pitch flexibility effect on flutter characteristics of wing-store configurations in transonic wind tunnel
TRANSONIC WIND TUNNEL↗
Pitch angle distributions and mirror point densities in the outer radiation zone
Pitch angle distributions and mirror point densities in outer radiation zone
ANGULAR DISTRIBUTION↗
Pitch angle distribution and mirror point densities in the outer radiation zone
Calculation of equatorial pitch angle distribution of trapped radiation from count rate of omnidirectional detector along line of force - mirror point density calculation
TRAPPED RADIATION↗
Some aspects of the flight dynamics of the aerobee 350 in region of pitch-roll coupling
Flight characteristics of Aerobee 350 rocket in region of pitch-roll coupling
COUPLING↗
Precritical calculations for the 2.9 in. pitch, twmr critical assembly
Critical loadings and precritical calculations for 2.9 inch pitch core in determining feasibility of isotopically enriched tungsten water moderated reactor for use as nuclear rocket
TUNGSTEN↗
Effect of pitch program variations on launch availability of Atlas/Centaur-AC-7 to AC-15
Pitch programs for Atlas Centaur vehicle launch times based on wind profile data
LAUNCH DATE↗
Transonic aerodynamic damping and oscillatory stability in yaw and pitch for a model of a variable-sweep supersonic transport airplane
Transonic aerodynamic stability and damping in yaw and pitch for variable sweep supersonic transport model
TRANSONIC SPEED↗
Experimentally Determined Effects of Varying Pitch and Control Stiffnesses on the Flutter Characteristics at Supersonic Speeds of All-movable Wing and Tail Models
Pitch and control stiffness effects on flutter characteristics of all-moveable wing and vertical and horizontal tails on fighter aircraft at supersonic speeds
FLUTTER↗
Aerobee 150 structural and aerodynamic pitch coupling
Aerobee 150 structural and aerodynamic pitch coupling failure analysis based on flight performance data reduction
FLIGHT CHARACTERISTICS↗
Pitch-angle dependence of first-order Fermi acceleration at shock fronts.
Pitch-angle dependence of first-order Fermi acceleration of particles trapped between shock front and moving magnetic mirror
PARTICLE ACCELERATION↗
Hovering performance characteristics of a rotor with and without blade-pitch servo-control flaps
Photographic performance evaluation of hovering helicopter rotor with and without blade pitch servocontrol flaps
HELICOPTER ROTOR↗