PHYSICAL AND CHEMICAL PROPERTIES OF HEXANITROETHANE
INTERNATIONAL CHEMICAL ENGINEERING
Digest of Translated Russian Literature: INTERNATIONAL CHEMICAL
TURBULENCE EFFECTS IN CHEMICAL REACTION KINETICS MEASUREMENTS
CONTOUR CALCULATIONS FOR CHEMICAL NONEQUILIBRIUM FLOW
CONTACT SURFACE TAILORING IN A CHEMICAL SHOCK TUBE
EQUIVALENCE BETWEEN CHEMICAL-REACTION AND VOLUMEVISCOSITY EFFECTS IN LINEARIZED NONEQUILIBRIUM FLOWS
Chemical nonequilibrium boundary layer
Chemical Scavenger Probes in Nonequilibrium Gasdynamics
Chemical and vibrational relaxation of an inviscid hypersonic flow
Chemical Kinetic Analysis of Rocket Exhaust Temperature Measurements
A quasi-one-dimensional treatment of chemical reactions in turbulent wakes of hypersonic objects
Nuclear-thermal vs chemical drives for superorbital velocities
Chemical nonequilibrium effects in hypersonic pure air wakes
Chemical pressurization of hypergolic liquid propellants
Chemical Nonequilibriuin Studies in Supersoiiic Nozzle Flows
Chemical and nozzle flow losses in hypersonic ramjets
Wave intersection limits for focused compression of air in chemical equilibrium
Velocity defect laws for transpired turbulent boundary layers
Characteristic calculation of flowfields with chemical reactions.
Comparison of chemical history and rates for the H sub 2 -air reaction.
Instrumental determination of large amounts of fluorine in oxygen.
Significance of nonequilibrium conductivity on plasma engine performance.
Thermal diffusivity of ammonium perchlorate.
Effects of grain configuration upon the burning rate of a spinning rocket motor.
Shock tube ignition delay studies of endothermic fuels.
Ignition of ammonium perchlorate composite propellants by convectiveheating.
Ignition of simulated propellants based on ammonium perchlorate.
A theory for ignition and deflagration of fuel drops.
Failure behavior of composite hydrocarbon fuel binder propellants.
Nonacoustic instability of composite propellant combustion.
Effect of liquid nitrogen dilution on LOX IMPACT sensitivity.
Including re-entry heating in rocket engine thermal analyses.
Temperature distribution within a particle during evaporation.
Computer experiments related to chemical propulsion.
Chemical relaxation phenomena behind normal shock waves in a dissociated freestream.
A simplified technique for evaluating vibrational and/or chemical relaxation behind shock waves.
Temperature sensitivity of solid propellant burning rate.
Influence of embedded metal fibers on solid- propellant burning rate.
Development of a fundamental model of hypergolic ignition in space-ambient engines.
Catalyzed thermal decomposition of ammonium perchlorate.
Control of pressure deflagration limits of composite solid propellants.
Internal ballistics of slotted-tube, solid- propellant rocket motors.
Application of the hydraulic analogy to axisymmetric nonideal compressible gas systems.
Dynamics of heterogeneous reaction at a stagnation point.
Characterization of volatilized species from solid propellants.
Effect of specific-heat ratio on mass flow for swirling nozzle flow.