Learning dominant physical processes with data-driven balance models. [PDF]
Callaham JL +4 more
europepmc +1 more source
Natural and Anthropogenic Sources of Seismic, Hydroacoustic, and Infrasonic Waves: Waveforms and Spectral Characteristics (and Their Applicability for Sensor Calibration). [PDF]
Schwardt M +4 more
europepmc +1 more source
FY 1989 scientific and technical reports, articles, papers, and presentations [PDF]
A compendium of bibliographic references to papers presented by Marshall Space Flight Center (MSFC) personnel and contractors during FY 1989 is provided.
Turner, Joyce E.
core +1 more source
Multidisciplinary Study of Pulse Detonation Engines [PDF]
Research at the Explosion Dynamics Laboratories at Caltech over the past three years under an ONR contract has examined many issues critical to Pulse Detonation Engine (PDE) development.
Shepherd, J. E.
core
Institute for Computational Mechanics in Propulsion (ICOMP) [PDF]
The Institute for Computational Mechanics in Propulsion (ICOMP) is a combined activity of Case Western Reserve University, Ohio Aerospace Institute (OAI) and NASA Lewis.
Feiler, Charles E.
core +1 more source
87th Annual Meeting of the Meteoritical Society 2025: Abstracts
Meteoritics &Planetary Science, Volume 60, Issue S1, Page 30-350, August 2025.
wiley +1 more source
Defining and Measuring Pressure Gain [PDF]
This presentation describes experimental and computational approaches to measuring pressure gain in the various devices currently under investigation wherein the working fluid undergoes a pressure gain combustion (PGC) process.
Paxson, Dan
core +1 more source
Aeronautical Engineering: A special bibliography with indexes, supplement 54 [PDF]
This bibliography lists 316 reports, articles, and other documents introduced into the NASA scientific and technical information system in January ...
core +1 more source
Nitrous Oxide/Ethanol Cylindrical Rotating Detonation Engine for Sounding Rocket Space Flight [PDF]
There are few experimental studies on rotating detonation engines (RDEs) with liquid propellants. This study reveals the static thrust performance of a cylindrical RDE with ethanol and liquid nitrous oxide as propellants under atmospheric pressure.
Eguchi, Hikaru +14 more
core +1 more source
Cost studies of multipurpose large launch vehicles. Volume 7 - Advanced technology implications Final report [PDF]
Advanced technology implications of multistage, multipurpose large launch ...
Corso, C. J.
core +1 more source

