New exact solutions of oblique detonations are developed for the supersonic irrotational flow of an inviscid calorically perfect ideal gas which undergoes a one-step, irreversible, exothermic, zero activation energy reaction as it passes through a straight shock over a curved wedge. A full exact solution gives expressions for the velocity, pressure, density, temperature, and position as parametric functions of a variable characterizing the extent of reaction. Three limiting cases are then studied in which all variables are obtained as functions of position. The first, obtained in the asymptotic high Mach number limit, gives a simple exponential form at leading order while confining the effects of heat release to higher order. An improvement is realized in the second asymptotic limit, which better accounts for finite heat release at the expense of a more elaborate form in terms of the Lambert W function. The third, obtained for a Chapman-Jouguet condition with no additional asymptotic limits, gives all variables in terms of the Lambert W function. The solutions provide a more compact and refined description of oblique detonation; moreover, they are in harmony with long-held understanding of such flows. As the simple model employed is a rational limit of models used in the computational simulation of complex supersonic reactive flows, the solutions can serve as benchmarks for mathematical verification of general computational algorithms. An example of such a verification is given by comparing the predictions a modern shock-capturing code to those of the full exact solution. The realized spatial convergence rate is 0.779, far less than the fifth order accuracy which the chosen algorithm would exhibit for smooth flows, but consistent with the predictions of all shock-capturing codes, which never converge with greater than first order accuracy for flows with embedded discontinuities.