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Sandwich Structures
1
Electronic Book
 

Acoustically tailored composite rotorcraft fuselage panels


Hambric, Stephen A., author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, July 2015. 2015-

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 Axe Federal Documents Online  NAS 1.26:2015-218769    ---  Available
2
ElectronicResource GovDoc
 

Aeroelastic sizing for high-speed research (HSR) longitudinal control alternatives project (LCAP)



Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2005] 2005

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 Axe Federal Documents Online  NAS 1.60:2005-213533    ---  Available
3
ElectronicResource GovDoc
 

Analytic and computational perspectives of multi-scale theory for homogeneous, laminated composite,



Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012] 2012

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 Axe Federal Documents Online  NAS 1.60:2012-217573    ---  Available
4
ElectronicResource GovDoc
 

An Approximate solution and master curves for buckling of symmetrically laminated composite cylinder


Nemeth, Michael P., author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2013. 2013

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 Axe Federal Documents Online  NAS 1.60:2013-217999    ---  Available
5
ElectronicResource GovDoc
 

Comparison of open-hole compression strength and compression after impact strength on carbon fiber/e


Hodge, A. J.
[Huntsville], Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2011] 2011

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 Axe Federal Documents Online  NAS 1.60:2011-216460    ---  Available
6
ElectronicResource GovDoc
 

Compression after impact experiments and analysis on honeycomb core sandwich panels with thin facesh


McQuigg, Thomas D.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011] 2011

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 Axe Federal Documents Online  NAS 1.26:2011-217157    ---  Available
7
ElectronicResource GovDoc
 

The effects of foam thermal protection system on the damage tolerance characteristics of composite s


Nettles, A. T. (Alan T.)
[Huntsville], Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2011] 2011

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 Axe Federal Documents Online  NAS 1.60:2011-216457    ---  Available
8
ElectronicResource GovDoc
 

An examination of impact damage in glass/phenolic and aluminum honeycomb core composite panels


Nettles, A. T. (Alan T.)
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, VA : For sale by the National Technical Information Service], 1990. 1990

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 Axe Federal Documents Online  NAS 1.60:3042    ---  Available
9
ElectronicResource GovDoc
 

Identification of crew-systems interactions and decision related trends


Jones, Sharon Monica, author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2013. 2013

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 Axe Federal Documents Online  NAS 1.60:2013-218000    ---  Available
10
Electronic Book
 

Mechanical property characterization of Borsic®/aluminum laminates at room and elevated temperatures


McWithey, Robert R., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980. 1980-

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 Axe Federal Documents Online  NAS 1.60:1761    ---  Available
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