Books on the topic 'Honeycomb structures'

C, Thompson Randolph, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Titanium honeycomb panel testing. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

C, Thompson Randolph, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Titanium honeycomb panel testing. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

Daigaku, Keiō Gijuku, HTA kenkyūkai, HTA Association, and Shinkenchikusha, eds. Hanikamu chūbu ākitekuchā tekunorojī bukku. Tōkyō: Shinkenchikusha, 2009.

Weichuan, Lin, Mbanefo Uy, and Langley Research Center, eds. Facesheet wrinkling in sandwich structures. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Walker, Sandra P. Evaluation of composite honeycomb sandwich panels under compressive loads at elevated temperatures. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

Bitzer, Tom. Honeycomb technology: Materials, design, manufacturing, applications and testing. London: Chapman & Hall, 1997.

M, Jensen, Grant L, and Langley Research Center, eds. High temperature be panel development. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

A, Ivanov A. Novoe pokolenie sotovykh zapolniteleĭ dli︠a︡ aviat︠s︡ionno-kosmicheskoĭ tekhniki. Moskva: Ėnergoatomizdat, 2000.

Endogur, A. I. Sotovye konstrukt͡s︡ii: Vybor parametrov i proektirovanie. Moskva: "Mashinostroenie", 1986.

Tao, Zhang. Study of impact damage of Nomex honeycomb sandwich plates. Harbin, Heilongjiang Province, China: School of Aeronautics, Harbin Institute of Technology, 1989.

Center, Langley Research, ed. High capacity demonstration of honecomb panel heat pipes. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

United States. National Aeronautics and Space Administration., ed. A modified VAPEPS method for predicting vibroacoustic response of unreinforced mass loaded honeycomb panels. [Washington, DC]: NASA, 1989.

United States. National Aeronautics and Space Administration., ed. A comparison of experimental and theoretical results for labyrinth gas seals with honeycomb stators. [Washington, DC]: National Aeronautics and Space Administration, 1988.

M, McGowan David. Compression response of a sandwich fuselage keel panel with and without damage. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

P, Willis B., Schoenenberger M, and United States. National Aeronautics and Space Administration., eds. Porous and microporous honeycomb composites as potential boundary-layer bleed materials. [Washington, D.C: National Aeronautics and Space Administration, 1997.

P, Willis B., Schoenenberger M, and United States. National Aeronautics and Space Administration., eds. Porous and microporous honeycomb composites as potential boundary-layer bleed materials. [Washington, D.C: National Aeronautics and Space Administration, 1997.

R, Horn J., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Geometric programming prediction of design trends for OMV protective structures. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Chamis, C. C. Fiber composite sandwich thermostuctural behavior, computationalsimulation. [Washington, DC]: National Aeronautics and Space Administration, 1986.

T, Nettles A., and George C. Marshall Space Flight Center., eds. A novel method of testing the shear strength of thick honeycomb composites. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

K, Hoffman Eric, and Langley Research Center, eds. Evaluation of the transient liquid phase (TLP) bonding process for Ti₃-Based honeycomb core sandwich structure. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

Schramm, David M. Understanding advanced composite & plastics repair concepts (basic). Oklahoma City, Okla: ADAIR Plastics and Composites, 1994.

Gibson, Lorna J. Cellular solids: Structure & properties. Oxford [Oxfordshire]: Pergamon Press, 1988.

Center, Langley Research, ed. Development of metallic thermal protection systems for the reusable launch vehicle. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

Kamo, Tsutomu, and Masao Yoshioka. Honeycomb dynamics architecture. [Tokyo]: Shinkenchiku-Sha, 2008.

Shideler, John L. Thermal and structural tests of Rene 41 honeycomb integral-tank concept for future space transportation systems. Hampton, Va: Langley Research Center, 1992.

L, Shideler John, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Thermal and structural tests of René 41 honeycomb integral-tank concept for future space transportation systems. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

Experimental evaluation of honeycomb/screen configurations and short contraction section for NASA Lewis Research Center's altitude wind tunnel. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

Fiedler, Thomas. Numerical and Experimental Investigation of Hollow Sphere Structures in Sandwich Panels. Trans Tech Publications, Limited, 2008.

An examination of impact damage in glass/phenolic and aluminum honeycomb core composite panels. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Compression response of a sandwich fuselage keel panel with and without damage. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Flow quality measurements in an aerodynamic model of NASA Lewis' icing research tunnel. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1999.

Von der Faser zum Haus: Das Potential von gefalteten Wabenplatten aus Papierwerkstoffen in ihrer architektonischen Anwendung. Weimar: Bauhaus-Universitätsverlag, in Jonas Verlag für Kunst und Literatur GmbH, 2017.

The beehive metaphor: From Gaudí to Le Corbusier. London: Reaktion, 2000.

Darrigol, Olivier. Models, structure, and generality in Clerk Maxwell’s theory of electromagnetism. Edited by Karine Chemla, Renaud Chorlay, and David Rabouin. Oxford University Press, 2017. http://dx.doi.org/10.1093/oxfordhb/9780198777267.013.12.

Hepburn, H. R., O. Duangphakdee, and C. W. W. Pirk. Honeybee Nests: Composition, Structure, Function. Springer Berlin / Heidelberg, 2016.

Hepburn, H. R., O. Duangphakdee, and C. W. W. Pirk. Honeybee Nests: Composition, Structure, Function. Springer London, Limited, 2014.

Pohl, Almut. Strengthened Corrugated Paper Honeycomb for Application in Structural Elements. vdf Hochschulverlag ETH Zurich, 2010.

National Aeronautics and Space Administration (NASA) Staff. Ambient Temperature Fatigue Tests of Elements of an Actively Cooled Honeycomb Sandwich Structural Panel. Independently Published, 2018.

National Aeronautics and Space Administration (NASA). Damage Tolerance Comparison of Composite Hat-Stiffened and Honeycomb Sandwich Structure for Launch Vehicle Interstage Applications. Independently Published, 2020.