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1

Ardema, Mark D. Optimization of supersonic transport trajectories. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1998.

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2

Roberts, Leonard. Computation of high speed transport aerodynamics. Stanford, Calif: Stanford University, Dept. of Aeronautics and Astronautics, 1991.

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3

Tavares, T. S. A supersonic fan equipped variable cycle engine for a Mach 2.7 supersonic transport. Cleveland, Ohio: Lewis Research Center, 1985.

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4

Iinkai, Sangyō Gijutsu Shingikai (Japan) Chōonsoku Yusōkiyō Suishin Shisutemu Hyōka. "Chōonsoku yusōkiyō suishin shisutemu" saishū hyōka hōkokusho. [Tokyo]: Sangyō Gijutsu Shingikai Hyōka Bukai Chōonsoku Yusōkiyō Suishin Shisutemu Hyōka Iinkai, 1999.

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5

Company, Douglas Aircraft. 1989 High-speed civil transport studies. Hampton, Va: Langley Research Center, 1991.

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6

Strack, William C. The challenges and opportunities of supersonic transport propulsion technology. [Washington, DC]: National Aeronautics and Space Administration, 1988.

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7

International, Workshop on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport (2000 Tokyo Japan). International Workshop on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport: 17-19 January 2000, Tokyo. Tokyo, Japan: National Aerospace Laboratory, 2000.

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8

Lessard, Victor R. Analysis of a high speed civil transport configuration at subsonic flow conditions using a Navier-Stokes solver. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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9

Concorde: Le magnifique. Toulouse: Privat, 2008.

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10

Concorde and the Americans: International politics of the supersonic transport. Washington, D.C: Smithsonian Institution Press, 1997.

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11

Concorde and the Americans: International politics of the supersonic transport. London: Airlife, 1997.

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12

Martin, Roderick H. Isothermal aging ofIM7/8320 and IM7/5260. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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13

Martin, Roderick H. Isothermal aging ofIM7/8320 and IM7/5260. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

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14

Cox, Timothy H. Evaluation of high-speed civil transport handling qualities criteria with supersonic flight data. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1997.

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15

High, Speed Commercial Flight Symposium (2nd 1988 Columbus Ohio). High speed commercial flight: From inquiry to action : proceedings of the Second High Speed Commercial Flight Symposium, Columbus, Ohio, October 19-20, 1988. Columbus, Ohio: Battelle Press, 1989.

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16

United States. Congress. House. Committee on Transportation and Infrastructure. Commercial operation of supersonic transport category aircraft: Report (to accompany H.R. 661) (including cost estimate of the Congressional Budget Office). [Washington, D.C: U.S. G.P.O., 1999.

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17

Rules, United States Congress House Committee on. Providing for the consideration of H.R. 661, Conditionally prohibiting the operation of supersonic aircraft: Report (to accompany H. Res. 86). [Washington, D.C: U.S. G.P.O., 1999.

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18

High Speed Commercial Flight Symposium (1st 1986 Columbus, Ohio). High speed commercial flight, the coming era: Proceedings of the First High Speed Commercial Flight Symposium, Columbus, Ohio, October 22-23, 1986. Columbus: Battelle Press, 1987.

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19

Keidel, Paul. The horizon: A blended wing aircraft configuration design project : NASA/USRA advanced design program, final report 1987-1988. Pomona, Calif: California State Polytechnic University Pomona, Aerospace Engineering Dept., 1988.

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20

Rules, United States Congress House Committee on. Providing for the consideration of H.R. 661, Conditionally prohibiting the operation of supersonic aircraft: Report (to accompany H. Res. 86). [Washington, D.C: U.S. G.P.O., 1999.

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21

Mann, Michael J. Design of supersonic transport flap systems for thrust recovery at subsonic speeds. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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22

Gall, Peter D. Study of an efficient long-range Mach 2.7 supersonic transport configuration concept. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

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23

Mann, Michael J. Design of supersonic transport flap systems for thrust recovery at subsonic speeds. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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24

Shaw, Robert J. Progress toward meeting the propulsion technology challenges for a 21st century high-speed civil transport. [Washington, D.C: National Aeronautics and Space Administration, 1997.

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25

Shaw, Robert J. Progress toward meeting the propulsion technology challenges for a 21st century high-speed civil transport. [Washington, D.C: National Aeronautics and Space Administration, 1997.

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26

Bhatt, R. S. Nonlinear stability of supersonic jets. Hampton, Va: NASA Langley Research Center, 1995.

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27

Cox, Timothy H. Longitudinal handling qualities of the Tu-144LL airplane and comparisons with other large, supersonic aircraft. Edwards, Cal: National Aeronautics and Space Administration, Dryden Flight Research Center, 2000.

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28

Lee, C. M. High speed commercial transport fuels considerations and research needs. [Washington, D.C: National Aeronautics and Space Administration, 1990.

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29

Shaw, Robert J. Engine technology challenges for a 21st century high speed civil transport. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.

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30

Schulz, Paul. Materials research for high speed civil transport and generic hypersonics: Metals durability. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

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31

Jacobson, Nathan S. High-temperature durability considerations for HSCT combustor. Cleveland, Ohio: Lewis Research Center, 1992.

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32

United, States Congress House Committee on Science Space and Technology Subcommittee on Transportation Aviation and Materials. National Aero-Space Plane Program: Joint hearing before the Subcommittee on Transportation, Aviation, and Materials of the Committee on Science, Space, and Technology and the Subcommittee on Research and Development of the Committee on Armed Services, U.S. House of Representatives, One hundredth Congress, first session, March 11, 1987. Washington: U.S. G.P.O., 1987.

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33

FEDERAL AVIATION ADMINISTRATION. Final environmental impact statement: Baltimore/Washington International Airport, extension of Runway 15L/33R. [Baltimore]: Maryland State Aviation Administration, 1989.

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34

Baysal, Oktay. Aerodynamic shape optimization directed toward a supersonic transport using sensitivity analysis: Final report for the period ended August 15, 1995. Norfolk, Va: Dept. of Aerospace Engineering, College of Engineering & Technology, Old Dominion University, 1995.

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35

Stambler, I. Supersonic Transport. Putnam Pub Group (L), 2000.

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36

L, Tweedt Daniel, Chima Rodrick V, and United States. National Aeronautics and Space Administration., eds. NASA Lewis supersonic throughflow fan program. [Washington, DC: National Aeronautics and Space Administration, 1990.

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37

Aviones Supersonicos/Supersonic Jets (Vehiculos De Alta Tecnologia). Rosen Publishing Group, 2003.

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38

United States. National Aeronautics and Space Administration., ed. Supersonic transport grid generation, validation, and optimization. [Washington, DC: National Aeronautics and Space Administration, 1995.

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39

National Research Council (U.S.). Committee on High Speed Research., ed. U.S. supersonic commercial aircraft: Assessing NASA's high speed research program. Washington, D.C: National Academy Press, 1997.

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40

(US), National Research Council. U.S. Supersonic Commercial Aircraft: Assessing NASA's High Speed Research Program. National Academies Press, 1997.

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41

The evolution of the high-speed civil transport. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

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42

Concorde Experience. National Museums Of Scotland, 2006.

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43

Richard, Hines, Gilkey Samuel, and United States. National Aeronautics and Space Administration., eds. Engine technology challenges for a 21st century high-speed civil transport. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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44

United States. National Aeronautics and Space Administration., ed. The leading edge 250: Oblique wing aircraft configuration project : final report 1987 - 88 : NASA/USRA advanced design program. Pomona, Calif: California State Polytechnic University, Pomona Aerospace Engineering Dept., 1988.

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45

United States. National Aeronautics and Space Administration., ed. Supersonic airplane study and design. San Jose, CA: MCAT Institute, 1993.

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46

United States. National Aeronautics and Space Administration., ed. Supersonic airplane study and design. San Jose, CA: MCAT Institute, 1993.

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47

The aerodynamic design of the oblique flying wing supersonic transport. Palo Alto, Calif: Stanford University, 1990.

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48

Supersonic Jets (Amato, William. High-Tech Vehicles.). PowerKids Press, 2002.

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49

National Research Council (U.S.). Committee on Breakthrough Technology for Commercial Supersonic Aircraft., ed. Commercial supersonic technology: The way ahead. Washington, D.C: National Academy Press, 2001.

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50

Integrated flight-propulsion control concepts for supersonic transport airplanes. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1990.

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