1. Boxer, E. (1967): Variable-Pitch supersonic inflow compressor and its application in a hypersonic engine. Conference on hypersonic aircraft technology, NASA SP-148, 401?416
2. Breugelmans, F. A. E. (1975): The supersonic axial inlet component in a compressor, ASME paper 75-GT-26
3. Crawley, E. F.; Hall, K. C. (1984): Optimization and mechanisms of mistuning of cascades, ASME paper 84-GT-196
4. Ferri, A. (1956): Problems related to matching turbojet engine requirements to inlet performances as functions of flight mach number and angle of attack, Air Intake Problems in Supersonic Propulsion, J. Fabri. Ed., AGARDograph No. 27, AGARD
5. Gorelov, D. N. (1966): Lattice of plates in an unsteady supersonic flow, Fluid Dynamics, Vol. 1, No. 4, 34?39