Supersonic flow past compression/expansion ramps represents a canonical problem in fluid dynamics which has been studied extensively in the past assuming perfect gas behaviour. More recently real gas effects on such flows have received increasing attention as part of efforts, among others, to increase the efficiency of Organic Rankine Cycles for decentralized power plants.Of special interest in this connection are dense gases of Bethe-Zel'dovich-Thompson fluids which have the distinguishing property that the so called fundamental derivative of gasdynamics Γ takes on negative values in the general neighbourhood of the thermodynamic critical point. Asymptotic analysis of the transonic flow regime has so far concentrated on cases where the unperturbed state with pressure p0, density ρ0 and entropy s0 is close to the transition curve Γ = 0 in the pressure specific volume plane such that |Γ0| 1, Λ0 = ρ ∂Γ ∂ρ s = O(1), Kluwick and Cox [1], [2]. These studies have revealed a number of new phenomena and a non-uniqueness of solutions exceeding that known from the theory of perfect gases.Here we extend the analysis to cover flows where the unperturbed state in the p, 1/ρ plane is in the vicinity of the point on the transition line where Γ and Λ vanish simultaneously. Such flows have |Γ0| 1, |Λ0| 1, N0 = ρ ∂Λ ∂ρ s = O(1) and are of considerable practical interest as isentropes that can be realized experimentally at present just barely enter the negative Γ region. Again an increased wealth of possible solutions is observed.Steady transonic flow past past two-dimensional ramps has recently been considered by Kluwick and Cox [1], [2]. Most important, the flow medium was taken to be a dense gas of Bethe-Zel'dovich-Thompson type which has the distinguishing property that the so called fundamental derivative Γ = 1 c ∂(ρc) ∂ρ s which is strictly positive for perfect gases may be negative in a region located in the general neighbourhood of the thermodynamic critical point. Here ρ, c, and s specify the fluid density, the speed of sound and the specific entropy. Also the thermodynamic state of the fluid was assumed to vary along an isentope which passes through the main portion of the negative Γ region. If stagnation conditions then are chosen such that critical conditions are reached near the high or low pressure branch of the transition line Γ = 0 then it was found that two of the three possible sonic states which may occur during isentropic expansion differ very little in the Mach number M versus specific volume v = 1/ρ plane which led to a number of flow phenomena not possible in dilute, i.e. perfect gases. Here we extend the analysis of Kluwick and Cox [2] to cover isentropes which just barely enter the negative Γ region. Then all three possible sonic states M = 1 almost collapse in the M, v-plane. Flows of this type may appear somewhat artificial at first sight. However, the use of dense gases as working fluids for Organic Rankine Cycles seems to offer a realistic possibility to increase the efficiency of decentralised power pl...