Failure mechanisms of laminates transversely loaded by bolt push-through /

Methodology for predicting the onset of widespread fatigue damage in lap-splice joints /
by: Newman, J. C.
Published: (1998)

Experimental measurement of structural power flow on an aircraft fuselage : progress report no. 6, Jan.-June 1989 /
by: Cuschieri, J. M. (Joseph M.)
Published: (1991)

Influence of an asymmetric ring on the modeling of an orthogonally stiffened cylindrical shell /
by: Rastogi, Naveen
Published: (1994)

NASA airframe structural integrity program /
by: Harris, Charles E.
Published: (1990)

An evaluation of the pressure proof test concept for thin sheet 2024-T3 /
Published: (1990)

Weight assessment for fuselage shielding on aircraft with open-rotor engines and composite blade loss /
by: Carney, Kelly S. (Kelly Scott)
Published: (2013)

Numerical study of three-dimensional separation and flow control at a wing-body junction : progress report for the period ended April 30, 1989 /
by: Lakshmanan, Balakrishnan, 1957-
Published: (1989)

Effect of flange bolt preload on space shuttle main engine high pressure oxidizer turbopump housing analysis /
by: Min, J. B.
Published: (1991)

Compressive testing of stitched frame and stringer alternate configurations /
by: Leone, Frank A., et al.
Published: (2016)

Evaluation of pressurization fatigue life of 1441 Al-Li fuselage panel /
by: Bird, R. Keith, et al.
Published: (1999)

Structural analysis of test flight vehicles for application of multifunctional energy storage system /
by: Mukhopadhyay, Vivek, et al.
Published: (2019)

Damage arresting composites for shaped vehicles : phase II final report /
Published: (2011)

A torque, tension, and stress corrosion evaluation of high strength A286 bolts /
by: Montano, J. W.
Published: (1986)

A torque, tension, and stress corrosion evaluation of high strength A286 bolts /
by: Montano, J. W.
Published: (1986)

Study for prediction of rotor/wake/fuselage interference /
by: Clark, D. R.
Published: (1985)

A summary of structural test and simulation results for Hawker 4000 composite fuselage hardware /
by: Littell, Justin D., et al.
Published: (2023)

Estimation of dynamic rotor loads for the rotor systems research aircraft : methodology development and validation /
by: Du Val, R. W.
Published: (1985)

Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure /
by: Harris, Charles E., 1950-, et al.
Published: (1996)

A study of the utilization of advanced composites in fuselage structures of commercial aircraft : final report /
Published: (1985)

A summary of results from two full-scale Fokker F28 fuselage section drop tests /
by: Littell, Justin D.
Published: (2018)

Vertical drop test of a transport fuselage section located forward of the wing /
by: Williams, M. Susan
Published: (1983)

Process sensitivity, performance, and direct verification testing of adhesive locking features /
by: Golden, Johnny L.
Published: (2012)

Experimental behavior of fatigued single stiffener PRSEUS specimens /
by: Jegley, Dawn C.
Published: (2009)

Development of quiet honeycomb panels /
by: Palumbo, Daniel L.
Published: (2009)

Design, optimization and evaluation of integrally stiffened Al 7050 panel with curved stiffeners /
Published: (2011)

PRSEUS panel fabrication final report /
by: Linton, Kim A.
Published: (2014)

Combining through-thickness reinforcement and self-healing for improved damage tolerance and durability of composites /
by: O'Brien, T. Kevin
Published: (2013)

Preload loss in a spacecraft fastener via vibration-induced unwinding /
by: DellaCorte, Christopher, et al.
Published: (2018)

Longitudinal weld land buckling in compression-loaded orthogrid cylinders /
by: Thornburgh, Robert P.
Published: (2010)

An application of retroduction to analyzing and testing the backing off of nuts and bolts during dynamic loading /
by: Kerley, James J.
Published: (1987)

Global/local stress analysis of composite panels /
by: Ransom, Jonathan B.
Published: (1989)

Simplified design procedures for fiber composite structural components/joints /
by: Murthy, P. L. N.
Published: (1990)

Computational analysis of the X-57 Maxwell airplane at unpowered conditions (preliminary fuselage) /
by: Deere, Karen A. (Karen Ann)
Published: (2022)

Composite transport wing technology development /
by: Madan, Ram C.
Published: (1988)

Identifying and characterizing discrepancies between test and analysis results of compression-loaded panels /
by: Thornburgh, Robert P.
Published: (2005)

Fuselage design for a specified Mach-sliced area distribution /
by: Barger, Raymond L.
Published: (1990)