Oxy-Acetylene Flame Types

Artificial gravity can be created in a spacecraft by rotating the structure. Occupants feel a centrifugal force pushing them towards the outer hull, mimicking gravity. The magnitude of this apparent gravity is given by \(a = \omega^2 r\), where \(\omega\) is the angular velocity and \(r\) is the radius of rotation. This is proposed to counteract the negative health effects of long-term weightlessness.

Oxy-acetylene welding uses a flame produced by the combustion of acetylene (\(C_2H_2\)) with pure oxygen. The reaction occurs in two stages. The primary reaction in the inner, white-hot cone is incomplete, producing carbon monoxide and hydrogen: \(2C_2H_2 + 2O_2 \rightarrow 4CO + 2H_2\). These hot gases then react with atmospheric oxygen in the outer envelope, completing the combustion.

A key property of TNT is its low melting point of 80.6 °C (177.1 °F), which is well below its autoignition temperature of 240 °C. This large temperature difference allows TNT to be safely melted using steam or hot water and poured into munitions casings, a process called melt-casting. This enables the production of dense, uniform, and crack-free explosive charges.

Gas cylinders for oxy-fuel welding store gases or other industrial or medical gases, at very high pressures. A pressure regulator is essential to reduce this to a safe, usable working pressure. A two-stage regulator performs this reduction in two steps, providing a highly constant delivery pressure even as the cylinder pressure drops with use. This ensures a stable flow, thus a stable flame for consistent weld quality.

The fire triangle is a simple model illustrating the three essential elements required for most fires: heat, fuel, and an oxidizing agent, typically atmospheric oxygen. Removing any one of these elements prevents a fire from starting or causes an existing fire to be extinguished. It is a fundamental concept in fire safety and prevention.

Delta-v, literally "change in velocity," is a scalar measure of the impulse required to perform an orbital maneuver. It quantifies the total propulsive effort needed for a mission, independent of the spacecraft's mass. This value is crucial for mission planning as it determines the necessary propellant load. Delta-v is cumulative; the total for a mission is the sum of all required maneuvers.

This equation describes the motion of vehicles that follow the basic principle of a rocket: a device that can apply acceleration to itself by expelling part of its mass with high velocity. It relates the delta-v a rocket can achieve to its effective exhaust velocity and the initial and final mass, given by \(\Delta v = v_e \ln \frac{m_0}{m_f}\).

Oxy-fuel cutting, or flame cutting, severs ferrous metals by a rapid, exothermic oxidation process. First, a preheating flame raises the steel's surface to its kindling temperature (approx. 870 °C or 1600 °F). A high-pressure jet of pure oxygen is then directed at the spot, initiating a chemical reaction, \(3Fe + 2O_2 \rightarrow Fe_3O_4\), which forms molten iron oxide (slag) and releases heat.

The separation factor, α (alpha), quantifies the selectivity of an extraction system for two different solutes, A and B. It is defined as the ratio of their individual distribution ratios, \(\alpha_{A,B} = \frac{D_A}{D_B}\). For a separation to be effective, α must be significantly different from unity. A larger α value implies an easier and more efficient separation.

The Log Mean Temperature Difference (LMTD) is the effective mean temperature difference for heat transfer in heat exchangers, particularly for counter-flow and parallel-flow arrangements. It is a logarithmic average of the temperature difference between the hot and cold fluids at each end. The LMTD is calculated using the formula: \(\Delta T_{LM} = \frac{\Delta T_A - \Delta T_B}{\ln(\Delta T_A / \Delta T_B)}\).

Temper embrittlement is a reduction in the toughness of certain alloy steels caused by holding them in, or slowly cooling them through, a specific temperature range (approximately 375–575 °C). This phenomenon is driven by the segregation of impurity elements (e.g., phosphorus, tin, antimony) to the grain boundaries, which weakens the cohesion between grains and promotes intergranular fracture.