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1

L, Sager Garrett, and United States. National Aeronautics and Space Administration., eds. Aircraft wing structure detail design. National Aeronautics and Space Administration, 1993.

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2

Wood, Robert. Aircraft observations of boundary layer structure. UMIST, 1997.

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3

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Aircraft propeller induced structure-borne noise. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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4

G, Rackl Robert, Andrianov Eduard V, and Langley Research Center, eds. Flight test measurements from the Tu-144LL structure/cabin noise experiment. National Aeronautics and Space Administration, Langley Research Center, 2000.

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5

McGarvey, Niall Sean. The impact of quality assurance on structural analysis within aircraft structure. The Author], 1996.

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6

Unruh, James F. Structure-borne noise estimates for the PTA aircraft. Langley Research Center, 1990.

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7

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Structure-borne noise estimates for the PTA aircraft. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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8

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Structure-borne noise estimates for the PTA aircraft. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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9

Ventresca, Rudolph. Organizational structure for Air National Guard tactical aircraft maintenance. Air University Press, 1991.

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10

Ventresca, Rudolph. Organizational structure for Air National Guard tactical aircraft maintenance. Air University Press, 1991.

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11

P, Woo E., and Langley Research Center, eds. Novel matrix resins for composites for aircraft primary structure. National Aeronautics and Space Administration, Langley Research Center, 1992.

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12

P, Woo E., and Langley Research Center, eds. Novel matrix resins for composites for aircraft primary structure. National Aeronautics and Space Administration, Langley Research Center, 1992.

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13

Alvin, Bayliss, Maestrello Lucio, and Institute for Computer Applications in Science and Engineering., eds. On the interaction of jet noise with a nearby flexible structure. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.

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14

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development., ed. Addendum to design manual for impact damage tolerant aircraft structure. AGARD, 1988.

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15

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Addendum to design manual for impact damage tolerant aircraft structure. s.n, 1988.

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16

Jorgensen, Charles C. Direct adaptive aircraft control using dynamic cell structure neural networks. National Aeronautics and Space Administration, Ames Research Center, 1997.

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17

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

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18

R, Bohne Alan. Storm precipitation and wind structure during aircraft strike lightning events. Atmospheric Sciences Division, Air Force Geophysics Laboratory, 1985.

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19

Bohne, Alan R. Storm precipitation and wind structure during aircraft strike lightning events. Atmospheric Sciences Division, Air Force Geophysics Laboratory, 1985.

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20

Office, General Accounting. European aeronautics: Strong government presence in industry structure and research and development support : report to Congressional requesters. The Office, 1994.

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21

Paul, Phillips A., and Phillips Thomas R, eds. Biz jets: Technology and market structure in the corporate jet aircraft industry. Kluwer Academic Publishers, 1994.

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22

Starke, E. A. NASA-UVa Light Aerospace Alloy and Structure Technology Program supplement: aluminum-based materials for high speed aircraft. Langley Research Center, 1993.

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23

Oum, Tae Hoon. Capital structure and socially optimal capacity in oligopoly: The case of airline industry. City University of Hong Kong, Department of Economics and Finance, 1997.

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24

Reardon, Lawrence F. Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature. Ames Research Center, 1989.

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25

United States. National Aeronautics and Space Administration., ed. Sound transmission through the walls of light aircraft: An investigation of structure-borne noise in a Handley Page 137 "Jetstream III" aircraft. Ray W. Herrick Laboratories, School of Mechanical Engineering, Purdue University, 1988.

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26

Halyo, Nesim. Integrated control using the SOFFT control structure. National Aeronautics and Space Administration, Langley Research Center, 1996.

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27

1944-, Birkler J. L., United States Navy, United States. Dept. of Defense., and National Defense Research Institute (U.S.), eds. The U.S. aircraft carrier industrial base: Force structure, cost, schedule, and technology issues for CVN 77. Rand, 1998.

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28

Office, General Accounting. Cruise missiles: Proven capability should affect aircraft and force structure requirements : report to Congressional committees. The Office, 1995.

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29

1935-, Smart D. F., and COSPAR, eds. Space life sciences: Structure and dynamics of the global space radiation field at aircraft altitudes. published for the Committee on Space Research [by] Pergamon, 2003.

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30

United States. National Aeronautics and Space Administration., ed. DIRECT ADAPTIVE AIRCRAFT CONTROL USING DYNAMIC CELL STRUCTURE NEURAL NETWORKS... NASA-TM-112198... OCT. 7, 1997. s.n., 1998.

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31

Center, Langley Research, ed. Mobility power flow analysis of an L-shaped plate structure subjected to acoustic excitation. National Aeronautics and Space Administration, Langley Research Center, 1989.

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32

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. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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33

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

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34

Reardon, Lawrence R. Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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35

Reardon, Lawrence R. Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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36

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. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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37

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Integrated design analysis and optimisation of aircraft structures: the material in this publication was assembled to support a Lecture Series under the sponsorhip of the Structure and Materials panel of AGARD and the Consultant and Exchange programme of AGARD presented on 8th-9th June 1992 in Pasadena, CA, United States, 22nd-23rd June 1992 in Lisbon, Portugal and 25th-26th June 1992 in London, United Kingdom. AGARD, 1992.

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38

Center, Langley Research, ed. Integrated control using the SOFFT control structure: Under contract NAS1-20185. National Aeronautics and Space Administration, Langley Research Center, 1996.

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39

Office, General Accounting. Navy carrier battle groups: The structure and affordability of the future force : report to the Congress. The Office, 1993.

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40

Development, North Atlantic Treaty Organization Advisory Group for Aerospace Research and. Analytical qualification of aircraft structures. AGARD, 1991.

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41

Cutler, John. Understanding aircraft structures. Collins, 1986.

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42

Cutler, John. Understanding aircraft structures. 3rd ed. Blackwell Science, 1999.

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43

Jeremy, Liber, ed. Understanding aircraft structures. 4th ed. Blackwell Pub., 2005.

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44

Young, Maurice I. Structural dynamics and vibrations of damped, aircraft-type structures. Langley Research Center, 1992.

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45

L, Chu Mamerto, and United States. National Aeronautics and Space Administration, eds. Structural properties of impact ices accreted on aircraft structures. National Aeronautics and Space Administration, 1987.

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46

Megson, T. H. G. Aircraft structures forengineering students. 2nd ed. Halsted Press, 1990.

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47

Development, North Atlantic Treaty Organization Advisory Group for Aerospace Research and. Analytical qualification of aircraft structures: Papers presented at the 70th Meeting of the Structures and Materials Panel of AGARD in Sorrento, Italy, 1st to 6th April 1990. AGARD, 1991.

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48

Niepokólczycki, Antoni. Fatigue of aircraft structures. Institute of Aviation Scientific Publications, 2009.

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49

Niepokólczycki, Antoni. Fatigue of aircraft structures. Institute of Aviation Scientific Publications, 2009.

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50

T, Sun C. Mechanics of aircraft structures. 2nd ed. John Wiley & Sons, 2006.

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