Approximate equations of motion of the gases produced by a laterally confined detonation(Approximate motion equations of gas flow behind detonation front in flat explosive plate covered by inert coating)
Theoretical basis of a design equation for determining the heat transfer coefficient during flow around a sphere in the range of Reynolds numbers from 30, 000 to 330, 000
Measurement of the wake velocity of a gas in a shock tube from the induced emf(Emf induced by plasma moving across constant transverse magnetic field used to determine rate of flow behind shock wave in shock tube)
Concerning the stabilization of detonation waves by means of poorly streamlined bodies(Stabilization of steady state detonation waves by means of bodies located in supersonic streams of combustible mixtures)
Local investigation of flows in the presence of shock and combustion waves by means of a new type of polar(Oblique shock-combustion wave polar investigation of stationary two dimensional flow of fuel mixture in compressed gas)
Measurements of the thermal conductivity of a diatomic gas in a shock tube(Temperature dependence of diatomic gases thermal conductivity coefficient from shock tube tests, noting molecular gases above dissociation temperature)
Measurement of relaxation effects in nozzle flows of hot combustion gases by means of a shock-tube device(Chemical relaxation effects in nozzle flow by measuring high temperatures created by detonation waves in shock tube, using hydrocarbon mixtures)
Accuracy of measurements of instantaneous gas- flow measurements by the two-heat-sensor method(Gas flow temperature measuring errors and accuracy, using two heat sensor method)