Zobrazeno 1 - 10 of 49 pro vyhledávání: '"Adam Przekop"'
1
Structural Response of a Stitched Composite Hybrid Wing Body Center Section
Autor: Marshall Rouse, Hsi-Yung T. Wu, Dawn C. Jegley, Andrew E. Lovejoy, Adam Przekop
Publikováno v: Journal of Aircraft. 58:580-590
Hybrid wing body is a fuel-efficient aircraft configuration where the pressurized center section is confined by almost-flat panels jointed at right angles. The combination of internal pressure and ...
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::709827ba66a611cd98d838e00e3cd4db
https://doi.org/10.2514/1.c035911
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3
Lessons Learned from Large-Scale Aerospace Structural Testing
Autor: Dawn C. Jegley, Andrew E. Lovejoy, Mark W. Hilburger, Adam Przekop
Publikováno v: AIAA Scitech 2021 Forum.
Large-scale testing of aerospace structures is frequently the final step in a development project to validate the structural performance, and that typically involves a large cost and time investment. In order to ensure that the testing provides the r
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::1f67d25c556c7ce09263f57023e95f4b
https://doi.org/10.2514/6.2021-1619
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6
Fabrication of a Composite Tow-Steered Structure for Air-Launch Vehicle Applications
Autor: Ray Grenoble, Peter D. Juarez, Dawn C. Jegley, Elizabeth D. Gregory, Martin J. McKenney, Leonard Oremont, Adam Przekop, Thuan Nguyen
Publikováno v: 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
Generation Orbit (GO) is developing the GO Launcher-1 (GO-1), a single stage liquid rocket that is launched from a Gulfstream III carrier aircraft platform. The vehicle is designed as the next generation platform for hypersonic flight testing and sub
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::6a44165e70d2c2756a0161cd13576472
https://doi.org/10.2514/6.2018-1376
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8
Vibroacoustic Tailoring of a Rod-Stiffened Composite Fuselage Panel with Multidisciplinary Considerations
Autor: Albert R. Allen, Adam Przekop
Publikováno v: Journal of Aircraft. 52:692-702
An efficient multi-objective design tailoring procedure seeking to improve the vibroacoustic performance of a fuselage panel while maintaining or reducing weight is presented. The structure considered is the pultruded rod stitched efficient unitized
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::c387ad41cd5ab0636ba6fb3439957faf
https://doi.org/10.2514/1.c033071
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9
Evaluation of a Metallic Repair on a Rod-Stiffened Composite Panel
Autor: Adam Przekop, Dawn C. Jegley
Publikováno v: Journal of Aircraft. 51:792-804
A design and analysis of a repair concept applicable to a stiffened composite panel based on the pultruded rod stitched efficient unitized structure was recently completed. The damage scenario considered was a midbay-to-midbay saw-cut with a severed
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::a07c78d290952e14b006f58676ddad95
https://doi.org/10.2514/1.c032461
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10
A review of indirect/non-intrusive reduced order modeling of nonlinear geometric structures
Autor: S. Michael Spottswood, Stephen A. Rizzi, Marc P. Mignolet, Adam Przekop
Publikováno v: Journal of Sound and Vibration. 332:2437-2460
The paper presents a review of reduced order modeling (ROM) techniques for geometrically nonlinear structures, more specifically of those techniques that are applicable to structural models constructed using commercial finite element software. The fo
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::6e64658d3b874dedaf3e4cc336118d07
https://doi.org/10.1016/j.jsv.2012.10.017
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