Results 51 to 60 of about 1,923 (153)

Learning dominant physical processes with data-driven balance models. [PDF]

open access: yesNat Commun, 2021
Callaham JL   +4 more
europepmc   +1 more source

FY 1989 scientific and technical reports, articles, papers, and presentations [PDF]

open access: yes
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]

open access: yes, 2002
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]

open access: yes
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

open access: yes
Meteoritics &Planetary Science, Volume 60, Issue S1, Page 30-350, August 2025.
wiley   +1 more source

Defining and Measuring Pressure Gain [PDF]

open access: yes
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]

open access: yes
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]

open access: yes
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

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