Study of a family of supersonic inlet systems.
Large scale axisymmetric inlet systems performance capabilities, reviewing theoretical and experimental programs
Cubbison, R. W.↗
Engineering topics
Smeltzer, D. B.
Publications and source records attributed to Smeltzer, D. B..
Investigation of a nearly isentropic mixed compression axisymmetric inlet system at Mach numbers 0.6 to 3.2
Wind tunnel tests of mixed-compression axisymmetric inlet system to determine bleed mass flow ratio, pressure recovery and pressure distortion
Smeltzer, D. B.↗
Investigation of a large-scale mixed compression axisymmetric inlet system capable of high performance at Mach numbers 0.6 to 3.0
Design and performance testing of large scale mixed compression axisymmetric inlet at transonic and supersonic speeds
Smeltzer, D. B.↗
Performance summary of a two-dimensional and an axisymmetric supersonic-inlet system
Explore the source record for details and available documents.
Sorensen, N. E.↗