CHARTERS et al., 1964 - Google Patents

High velocity guns for free-flight ranges(Guns with constant acceleration developed for firing aerodynamic models in high velocity flight research)

CHARTERS et al., 1964

Document ID
15242791831590876550
Author
CHARTERS A
CURTIS J
Publication year

External Links

Continue reading at scholar.google.com (other versions)

Similar Documents

Publication Publication Date Title
CHARTERS et al. High velocity guns for free-flight ranges(Guns with constant acceleration developed for firing aerodynamic models in high velocity flight research)
CHARTERS et al. Free-flight test apparatus- gas gun for study of hypersonic flight with hypervelocity projectile
BOUCHER et al. The sequential spark technique- A tool for wake velocity studies in ballistic ranges(Sequential electric spark technique for hypervelocity projectiles turbulent wake velocity measurements at ballistic ranges in free flight regime)
CERESUELA et al. Kinetic heating on a representative model of a supersonic transport aircraft< echauffement cinetique d'une maquette schematique d'avion de transport supersonique/(Kinetic heating on supersonic transport aircraft model sweptback delta wing in wind tunnel)
FRYNTA Influence of pitching during the passage of an aeroplane through a gust on the acceleration in its center of gravity(Pitching effect on aircraft gravity center during passage through gust, noting autopilot effect on tail assembly)
KUECHEMANN Hypersonic aircraft and their aerodynamic problems(Hypersonic aircraft and aerodynamic aspects for global transport operation noting shock waves, Mach number and gas dynamics)
DRINKWATER Flight experience with the OGEE wing at low speed(Flight experience with Ogee wing at low speed)
GYR Droplet motion in a turbulent field, showing that small radii droplets move with the same velocity distribution as the air moving them
FAINBERG Solution of the problem regarding the influence of hills on the steady motion of cold air(Characteristics method applied to aero- and hydrodynamics equations for motion of cold air mass, intersecting a mountain range)
LOMONACO Introduction to the problem of weightlessness in spaceflight and of the transition from accelerations to weightlessness and vice versa- Synthesis of the results obtained on man and animals by means of a subgravity tower and a subgravity axis(Subgravity tower and axis results obtained on man and animals, discussing transition from acceleration to weightlessness and vice versa)
BULL et al. Aerospace application of gun launched projectiles and rockets(Project High Altitude Research Program/HARP/ DIRECTED toward use of guns for scientific probing of upper atmosphere)
RAY et al. Longitudinal aerodynamic characteristics at Mach numbers from 0. 50 to 1. 19 of a supersonic transport model with a modified M wing(Longitudinal aerodynamic characteristics at Mach numbers 0. 50 to 1. 19 of supersonic transport model with modified M wing)
KUCHERMANN Characteristic configurations for supersonic aircraft with specific flight requirements
BREVIG A comparison between the ejector ramjet and the ducted rocket(Ejector ramjet and ducted rocket evaluation by analytical models for various flight trajectories, noting specific impulse improvement)
SCHINDELIN On the analog computer simulation of the motion of the centre of gravity of a guided stabilized missile in space(Analog simulation of guided stabilized missile center of gravity motion in space)
VERNHES Direct digital control of numerous engine functions by a single computer(Digital computer CPU control of kinetic heating processes in engine of supersonic aircraft under simulated flight conditions)
SEREBRENY Meteorological aspects such as temperature, cloud formation and transition altitudes of the supersonic transport problem
LANCASTER et al. Investigation of the aerodynamic characteristics of a 0. 02-scale model of the x-15 airplane at mach numbers of 2. 96, 3. 96, and 4. 65 at high angles of attack(Longitudinal and lateral aerodynamic characteristics of scale model of X-15 aircraft at high angles of attack)
STRAKHOVICH Total energy, mass laws, and first law of thermodynamics used to derive equations of streamline motion and gas dynamics
LACY et al. Evaluation and analysis of thrust units for power-limited propulsion systems(Velocity distribution of propellant ejection and effect on propulsion efficiency of ion engines)
KRUCZYNSKI et al. Sight line autopilot- A new concept in air weapons(Sight line autopilot/SLAP/ for side-firing aircraft pointing accuracy improvement, using optimal regulator theory to generate control gains)
BARCHE et al. Jet influence on V/STOL-aircraft in the transitional and high speed flight regime(Jet influence on V/STOL aircraft in transitional and high speed flight regime)
CERCIGNANI et al. Rayleigh's problem at low Mach numbers according to kinetic theory(Rayleigh problem at low Mach numbers and arbitrary Knudsen number investigated in rarefied gas dynamics according to kinetic theory)
HUNTER et al. Velocity requirements and transport costs for ferrying astronomical equipment into space, and problems with regard to telescopes
CARTER Technological contributions of the ch-53 a weapons system development program(Ch-53 a helicopter design optimization and selection discussing rotor system, airframe, power plant and stability in high speed flying)