Evaluation of pressurization fatigue life of 1441 Al-Li fuselage panelFormat: [microform] /
Author: Bird, R. Keith.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1999] This title can be found in 1 Iowa libraries.
Crashworthy evaluation of a 1/5-scale model composite fuselage conceptFormat: [microform] /
Author: Jackson, Karen E.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1999] This title can be found in 2 Iowa libraries.
Vibro-acoustics modal testing at NASA Langley Research CenterFormat: [microform] /
Author: Pappa, Richard S.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1999] This title can be found in 2 Iowa libraries.
Response of composite fuselage sandwich side panels subjected to internal pressure and axial tensionFormat: [microform] /
Publisher: [Washington, D.C. : National Aeronautics and Space Administration ;
Date: 1998] This title can be found in 1 Iowa libraries.
Methodology for predicting the onset of widespread fatigue damage in lap-splice jointsFormat: [microform] /
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1998] This title can be found in 1 Iowa libraries.
Analysis and design of fuselage structures including residual strength prediction methodology final report for NASA grant NAG-1-1588 /Format: [microform] :
Author: Knight, Norman F.
Publisher: [Norfolk, Va.] : Old Dominion University Research Foundation ;
Date: 1998] This title can be found in 2 Iowa libraries.
Compression response of a sandwich fuselage keel panel with and without damageFormat: [microform] /
Author: McGowan David M.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1997] This title can be found in 1 Iowa libraries.
Analytical studies of boundary layer generated aircraft interior noiseFormat: [microform] /
Author: Howe, M. S.
Publisher: Boston, MA : Boston University, College of Engineering ;
Date: 1997] This title can be found in 2 Iowa libraries.
Rotor-fuselage interactionsFormat: [microform] /
Author: Barry, John D.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1997] This title can be found in 2 Iowa libraries.
The characteristics of fatigue damage in the fuselage riveted lap splice jointFormat: [microform] /
Author: Piascik, Robert S.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1997] This title can be found in 2 Iowa libraries.
Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structureFormat: [microform] /
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1996] This title can be found in 1 Iowa libraries.
Nonlinear response and residual strength of damaged stiffened shells subjected to combined loadsFormat: [microform] /
Publisher: [Washington, D.C. : National Aeronautics and Space Administration ;
Date: 1996] This title can be found in 2 Iowa libraries.
Novel composites for wing and fuselage applications textile reinforced composites and design guidelines /Format: [microform] :
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1996] This title can be found in 2 Iowa libraries.
Novel composites for wing and fuselage applications. Task 1.Format: [microform] /
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1996] This title can be found in 2 Iowa libraries.
A record of all marker bands found in the upper rivet rows of 2 adjacent bays from a fuselage lap splice jointFormat: [microform] /
Author: Willard, Scott A.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1995] This title can be found in 2 Iowa libraries.
Novel composites for wing and fuselage applicationsFormat: [microform] /
Author: Sobel, Larry.
Publisher: [Washington, D.C. : National Aeronautics and Space Administration ;
Date: 1995] This title can be found in 2 Iowa libraries.
A review of ice accretion data from a model rotor icing test and comparison with theory /Author: Britton, Randall K.
Publisher: [Washington, DC] : National Aeronautics and Space Administration,
Date: [1991] This title can be found in 1 Iowa libraries.
Fuselage shell and cavity response measurements on a DC-9 test section /Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,
Date: [1991] This title can be found in 1 Iowa libraries.
A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas /Author: Mack, Robert J.
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division,
Date: 1990. This title can be found in 1 Iowa libraries.
Aircraft interior noise reduction by alternate resonance tuning : progress report for the period ending December, 1988 /Publisher: Durham, N.C. : Department of Mechanical Engineering and Materials Science, Duke University ;
Date: [1989] This title can be found in 1 Iowa libraries.
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