1. Heat transfer from a hemisphere cylinder equipped with flow separation spikes;Stalder,1954
2. Reduction in temperature-recovery factor associated with pulsating flows generated by spike-nosed cylinders at a Mach number of 3.50;Hermach,1957
3. Investigation of the flow over a spiked-nose hemisphere cylinder;Crawford,1959
4. Flowfield around spike-tipped bodies for high attack angles at Mach 4.5;Gnemmi;J. Propuls. Power,2003
5. Role of aerodome in pulsation/oscillation control and aeroheating reduction;Qin;Acta Astronaut.,2019