Books on the topic 'Composite aircraft structure'

Chamis, C. C. Structural tailoring of select fiber composite structures. [Washington, D.C.]: NASA, 1990.

Leite Cavalcanti, Welchy, Kai Brune, Michael Noeske, Konstantinos Tserpes, Wiesław M. Ostachowicz, and Mareike Schlag, eds. Adhesive Bonding of Aircraft Composite Structures. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-319-92810-4.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Repair of Aircraft Structures Involving Composite Materials. S.l: s.n, 1986.

Dastin, Samuel J. Aircraft composite materials and structures: Seminar notes. Lancaster, PA: Technomic Publishing Co., 1986.

Smith, Peter J. Damage tolerant composite wing panels for transport aircraft. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Renaud, Guillaume. Advanced optimal design concepts for composite material aircraft repair. [Downsview, Ont.]: University of Toronto, Institute for Aerospace Studies, 2003.

Poon, C. A review of crashworthiness of composite aircraft structures. Ottawa: National Aeronautical Establishment, 1990.

Development, Advisory Group for Aerospace Research and. The repair of aircraft structures involving composite materials. Neuilly-sur-Seine: Agard, 1986.

Development, North Atlantic Treaty Organization Advisory Group for Aerospace Research and. Composite repair of military aircraft structures: Papers presented at the 79th Meeting of the AGARD Structures and Materials Panel, held in Seville, Spain 3-5 October 1994. Neuilly sur Seine, France: AGARD, 1995.

Glossop, N. D. W. Optical fibre damage detection for an aircraft composite leading edge. [S.l.]: [s.n.], 1990.

Lameris, J. The use of load enhancement factors in the certification of composite aircraft structures. Amsterdam: National Aerospace Laboratory, 1990.

Mabson, Gerald E. Analysis and testing of composite aircraft frames for interlaminar tension failure. [S.l.]: [s.n.], 1988.

J, Smith P. Development of pressure containment and damage tolerance technology for composite fuselage structures in large transport aircraft. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1989.

Carden, Huey D. Unique failure behavior of metal/composite aircraft structural components under crash type loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Hai, Wang, and Chen Xiuhua, eds. Fei ji fu he cai liao jie gou qaing du fen xi: Strength analysis of composite aircraft structures. Shanghai Shi: Shanghai jiao tong da xue chu ban she, 2011.

Carden, Huey D. Failure behavior of generic metallic and composite aircraft structural components under crash loads. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Gangloff, R. P. NASA-UVa Light Aerospace Alloy and Structures Technology Program (LA2ST): A progress report, January 1, 1991 to June 30, 1991. Charlottesville, VA: School of Engineering & Applied Science, University of Virginia, 1991.

Gangloff, R. P. NASA-UVa Light Aerospace Alloy and Structures Technology Program (LA2ST): A progress report, January 1, 1991 to June 30, 1991. Charlottesville, VA: School of Engineering & Applied Science, University of Virginia, 1991.

Carden, Huey D. Failure behaviour of generic metallic and composite aircraft structural components under crash loads. Washington D.C: National Aeronautics and Space Administration Scientific and Technical Information Division, 1990.

Shah, C. H. Pin bearing evaluation of LTM25 composite materials. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

Loewy, Robert G. Composite structural materials: Semi-annual progress report, September 30, 1984 through April 30, 1985. Troy, N.Y: Rensselaer Polytechnic Institute, 1985.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. The utilization of advanced composites in military aircraft: Papers presented at the 73rd Meeting of the AGARD Structures and Materials Panel, held in San Diego, CA, United States, 7th-11th October 1991. Neuilly sur Seine, France: AGARD, 1992.

Deets, Dwain A. HiMAT flight program: Test results and program assessment overview. Edwards, Calif: Ames Research Center, 1986.

Jones, R., A. A. Baker, and L. R. F. Rose. Advances in the Bonded Composite Repair of Metallic Aircraft Structure. Elsevier Science, 2002.

A, Baker A., Rose L. R. F, and Jones R, eds. Advances in the bonded composite repair of metallic aircraft structure. Amsterdam: Elsevier, 2002.

Jones, R., A. A. Baker, and L. R. F. Rose. Advances in the Bonded Composite Repair of Metallic Aircraft Structure. Elsevier Science, 2002.

A, Baker A., Rhys Jones, and L. R. F. Rose. Advances in the Bonded Composite Repair of Metallic Aircraft Structure. Elsevier Science & Technology Books, 2003.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. NASA-UVa light aerospace alloy and structure technology program supplement: Aluminum-based materials for high speed aircraft. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Center, Langley Research, ed. NASA-UVa light aerospace alloy and structure technology program supplement: Aluminum-based materials for high speed aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

NASA-UVa light aerospace alloy and structure technology program supplement: Aluminum-based materials for high speed aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

NASA-UVa light aerospace alloy and structure technology program supplement: Aluminum-based materials for high speed aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

NASA-UVa light aerospace alloy and structure technology program suppleyment: Aluminum-based materials for high speed aircraft. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. NASA-UVa light aerospace alloy and structure technology program suppleyment: Aluminum-based materials for high speed aircraft. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

H, Middleton D., ed. Composite materials in aircraft structures. Burnt Mill, Harlow, Essex, England: Longman Scientific & Technical, 1990.

C, Hoskin B., and Baker A. A, eds. Composite materials for aircraft structures. New York, N.Y: American Institute of Aeronautics and Astronautics, 1986.

Dastin, Samuel J. Aircraft Composite Materials and Structures. Technomic Pub Co, 1986.

Scott, Murray L., and Alan Baker. Composite Materials for Aircraft Structures. American Institute of Aeronautics & Astronautics, 2016.

Middleton, Don. Composite Materials in Aircraft Structures. Wiley & Sons, Incorporated, John, 1990.

Development of thermoplastic composite aircraft structures. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Flight service evaluation of advanced composite ailerons on the L-1011 transport aircraft: Fourth annual flight service report. Burbank, Calif: Lockheed-California Co., 1986.

Center, Langley Research, ed. Flight service evaluation of advanced composite ailerons on the L-1011 transport aircraft: Fifth annual flight service report. Burbank, Calif: Lockheed-California Co., 1987.

Aircraft composite materials and structures: Seminar notes. Bethpage, N.Y: Grumman Corp., Aircraft Systems Division, 1986.

United States. National Aeronautics and Space Administration., ed. The design of composite structures: Aircraft design. Washington, DC: National Aeronautics and Space Administration, 1987.

Advanced Organic Composite Materials for Aircraft Structures. Washington, D.C.: National Academies Press, 1987. http://dx.doi.org/10.17226/19186.

Crashworthy Composite Structures: Aircraft and Vehicle Applications. DEStech Publications, Incorporated, 2020.

Composite chronicles: A study of the lessons learned in the development, production, and service of composite structures. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Critical joints in large composite primary aircraft structures. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1988.

Composite Materials For Aircraft Structures (Aiaa Education Series.). 2nd ed. AIAA (American Institute of Aeronautics & Ast, 2004.

Critical joints in large composite primary aircraft structures. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1988.

(Editor), Alan A. Baker, Stuart Dutton (Editor), and Donald Kelly (Editor), eds. Composite Materials for Aircraft Structures (Aiaa Education Series). 2nd ed. AIAA (American Institute of Aeronautics & Ast, 2004.