Design and Experimental Study of an Over-Under TBCC Exhaust System. [PDF]
Mo J, Xu J, Zhang L.
europepmc +1 more source
Advanced supersonic propulsion study, phase 3 [PDF]
The variable stream control engine is determined to be the most promising propulsion system concept for advanced supersonic cruise aircraft. This concept uses variable geometry components and a unique throttle schedule for independent control of two flow
Howlett, R. A. +3 more
core +1 more source
Tandem Fan Applications in Advanced STOVL Fighter Configurations [PDF]
The series/parallel tandem fan engine is evaluated for application in advanced STOVL supersonic fighter aircraft. Options in engine cycle parameters and design of the front fan flow diverter are examined for their effects on engine weight, dimensions ...
Eskey, Megan A. +2 more
core +1 more source
Ablative response of a silica phenolic to simulated liquid propellant rocket engine operating conditions [PDF]
Ablative response of silica phenolic to simulated liquid propellant rocket engine operating ...
Moyer, C. B. +3 more
core +1 more source
Proceedings to the 60th Annual Conference of the Particle Therapy Cooperative Group: 27 June - 2 July, 2022, Hosted by Miami Cancer Institute, part of Baptist Health South Florida, Miami, FL, USA. [PDF]
europepmc +1 more source
The NASA research program on propulsion for supersonic cruise aircraft [PDF]
The objectives and status of the propulsion portion of a program aimed at advancing the technology and establishing a data base appropriate for the possible future development of supersonic cruise aircraft are reviewed.
Weber, R. J.
core +1 more source
Recent Progress in Inkjet-Printed Thin-Film Transistors. [PDF]
Chung S, Cho K, Lee T.
europepmc +1 more source
Free-jet investigation of mechanically suppressed, high radius ratio coannular plug model nozzles [PDF]
The experimental and analytical acoustic results of a scale-model investigation or unsuppressed and mechanically suppressed high-radius ratio coannular plug nozzles with inverted velocity and temperature profiles are summarized.
Brausch, J. F. +3 more
core +1 more source
Evaluation of the Thermal Diffusivity of Carbon/Phenolic Composites (CPCs) through Oxy-Acetylene Torch (OAT) Test-Part 1: Experimental Characterization and Preliminary Validation. [PDF]
Natali M, Torre L, Rallini M.
europepmc +1 more source
Variable stream control engine concept for advanced supersonic aircraft: Features and benefits [PDF]
The Variable Stream Control Engine is studied for advanced supersonic cruise aircraft. Significant environmental and performance improvements relative to first generation supersonic turbojet engines are cited.
Howlett, R. A.
core +1 more source

