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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

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At least 307 records · Page 17

All sources NASA NTRS DOE OSTI

DOE OSTI2024

A Fixed-Step Under Frequency Load Shedding Scheme based on Load Criticality

Presentation for NAPS paper

Jimenez Aparicio, Miguel↗

DOE OSTI2025

High-Fidelity Self-Learning Tool for Residential Load and Load Flexibility Forecasting

In this project, we developed a set of high-fidelity modeling and optimization algorithms to enable conversion of individual homes into grid-integrated buildings, and a community of homes into a virtual power plant (VPP).

24 POWER TRANSMISSION AND DISTRIBUTION↗

DOE OSTI2017

Evaluating the Performance of Fasteners Subjected to Multiple Loadings and Loadings Rates and Identifying Sensitivities of the Modeling Process.

Abstract not provided.

Mersch, John Philip↗

DOE OSTI2018

Modeling Empirical Size Relationships on Load-Displacement Behavior and Failure in Threaded Fasteners.

Abstract not provided.

Grimmer, Peter W↗

NASA NTRS1964

Research investigations of bulkhead cylindri- cal junctions exposed to combined load, cryogenic temperature. part iii- theoretical analysis of the thermal loads

Thermal stress in thin walled shell joint of missile intertank

THERMAL STRESS↗

NASA NTRS1965

Note on individual storage loads and individual load reductions

Human recall of sequential memory tasks

MEMORY↗

NASA NTRS1965

Analytical procedure for determining random load acting on a spacecraft due to a primary random load acting on an exterior structure Quarterly report no. 2, 1 Sep. - 30 Nov. 1965

Sound and vibration transmission in OGO SPACECRAFT shroud system

STRUCTURAL VIBRATION↗

NASA NTRS1974

Computer program for buckling loads of orthotropic laminated stiffened panels subjected to biaxial in-place loads (BUCLASP 2)

General-purpose program performs exact instability analyses for structures such as unidirectionally-stiffened, rectangular composite panels. Program was written in FORTRAN IV and COMPASS for CDC-series computers.

Viswanathan, A. V.↗

NASA NTRS1979

Composite components under impact load and effects of defects on the loading capacity

Investigations were carried out on a horizontal tail assembly made of carbon fiber reinforced plastic for the Alpha Jet. The possibility of obtaining a leading edge nose design lighter but not more expensive than a metal version was studied. An important consideration was sufficient resistance of the leading edge against impact of stones and hailstones combined with high degree of stiffness. The improvement of energy reception characteristics of the materials through suitable laminate design was considered. Since certain defects occur in structural components, the effects of such defects on the characteristics of the parts were also studied.

Aoki, R.↗

NASA NTRS1982