Penetration of gaseous jets injected into a supersonic stream.

1966/11/01 by JOSEPH A. SCHETZ, Joseph A. Schetz, F. S. Billig +1 · 289 citations
Engineering · Physics and Astronomy · #Aerospace #Aerospace engineering #Combustion and Detonation Processes #Computational Fluid Dynamics and Aerodynamics #Computer science #Engineering #Laser-Plasma Interactions and Diagnostics #Mechanical engineering #Missile #Operations research #Penetration (warfare) #Physics #Propellant #Space (punctuation) #Space environment #Space research #Space technology #Spacecraft #Spacecraft design #Supersonic speed #Systems engineering

paper · doi:10.2514/3.28721

published in Journal of Spacecraft and Rockets 3(11), 1658-1665 (American Institute of Aeronautics and Astronautics)

openalex publication_date 1966/11/01 · openalex created_date 2025/10/10 · openalex updated_date 2026/07/29

Abstract

Covers advancements in spacecraft and tactical and strategic missile systems, including subsystem design and application, mission design and analysis, materials and structures, developments in space sciences, space processing and manufacturing, space operations, and applications of space technologies to other fields.

Cited by

• The Interaction of Jets with Crossflow
• Characteristics of Dual Transverse Injection in Scramjet Combustor, Part 1: Mixing

Related

• Experimental Investigation of Super- and Hypersonic Jet Interaction on Missile Configurations
• Three-Component Force Measurements on a Large Scramjet in a Shock Tunnel
• High velocity atomic oxygen/surface accommodation studies
• Integral-Rocket Dual-Combustion Ramjets: A New Propulsion Concept
• Supersonic/Hypersonic Flutter and Postflutter of Geometrically Imperfect Circular Cylindrical Panels