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Title: 3-D inelastic analysis methods for hot section components. Volume 1: Special finite element models. Annual status report, 14 February 1985-14 February 1986

Abstract

This annual status report presents the results of work performed during the third year of the 3-D Inelastic Analysis Methods for Hot Section Components program (NASA Contract NAS3-23697). The objective of the program is to produce a series of new computer codes that permit more accurate and efficient three-dimensional analysis of selected hot section components, i.e., combustor liners, turbine blades, and turbine vanes. The computer codes embody a progression of mathematical models and are streamlined to take advantage of geometrical features, loading conditions, and forms of material response that distinguish each group of selected components. This report is presented in two volumes. Volume 1 describes effort performed under Task 4B, Special Finite Element Special Function Models, while Volume 2 concentrates on Task 4C, Advanced Special Functions Models.

Authors:
Publication Date:
Research Org.:
Pratt and Whitney Aircraft, East Hartford, CT (USA)
OSTI Identifier:
6179354
Report Number(s):
N-87-22996; NASA-CR-179494; NAS-1.26:179494; PWA-5940-46-VOL-1; ASR-3
Resource Type:
Technical Report
Country of Publication:
United States
Language:
English
Subject:
42 ENGINEERING; COMBUSTION CHAMBERS; STRESS ANALYSIS; COMPUTER CODES; FINITE ELEMENT METHOD; TURBINE BLADES; BUCKLING; CREEP; HIGH TEMPERATURE; LINERS; MECHANICAL VIBRATIONS; THEORETICAL DATA; VANES; DATA; INFORMATION; MECHANICAL PROPERTIES; NUMERICAL DATA; NUMERICAL SOLUTION; 421000* - Engineering- Combustion Systems

Citation Formats

Nakazawa, S. 3-D inelastic analysis methods for hot section components. Volume 1: Special finite element models. Annual status report, 14 February 1985-14 February 1986. United States: N. p., 1987. Web.
Nakazawa, S. 3-D inelastic analysis methods for hot section components. Volume 1: Special finite element models. Annual status report, 14 February 1985-14 February 1986. United States.
Nakazawa, S. 1987. "3-D inelastic analysis methods for hot section components. Volume 1: Special finite element models. Annual status report, 14 February 1985-14 February 1986". United States.
@article{osti_6179354,
title = {3-D inelastic analysis methods for hot section components. Volume 1: Special finite element models. Annual status report, 14 February 1985-14 February 1986},
author = {Nakazawa, S},
abstractNote = {This annual status report presents the results of work performed during the third year of the 3-D Inelastic Analysis Methods for Hot Section Components program (NASA Contract NAS3-23697). The objective of the program is to produce a series of new computer codes that permit more accurate and efficient three-dimensional analysis of selected hot section components, i.e., combustor liners, turbine blades, and turbine vanes. The computer codes embody a progression of mathematical models and are streamlined to take advantage of geometrical features, loading conditions, and forms of material response that distinguish each group of selected components. This report is presented in two volumes. Volume 1 describes effort performed under Task 4B, Special Finite Element Special Function Models, while Volume 2 concentrates on Task 4C, Advanced Special Functions Models.},
doi = {},
url = {https://www.osti.gov/biblio/6179354}, journal = {},
number = ,
volume = ,
place = {United States},
year = {Sun Mar 01 00:00:00 EST 1987},
month = {Sun Mar 01 00:00:00 EST 1987}
}

Technical Report:
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