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1

J, Glassman Arthur, and United States. National Aeronautics and Space Administration., eds. Turbomachinery technology for high-speed civil flight. [Washington, DC]: National Aeronautics and Space Administration, 1989.

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2

Center, NASA Glenn Research, ed. Pulse detonation engines for high speed flight. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.

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3

1936-, Thornton Earl A., ed. Thermal structures and materials for high-speed flight. Washington, DC: American Institute of Aeronautics and Astronautics, 1992.

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4

Loquercio, Antonio. Agile Autonomy: Learning High-Speed Vision-Based Flight. Cham: Springer Nature Switzerland, 2023. http://dx.doi.org/10.1007/978-3-031-27288-2.

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5

Center, Langley Research, ed. Multivariable techniques for high-speed research flight control systems. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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6

Center, Ames Research, and United States. Army Aviation Research and Technology Activity., eds. Wake model for helicopter rotors in high speed flight. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

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7

1940-, Wilson John W., and Langley Research Center, eds. Radiation safety aspects of commercial high-speed flight transportation. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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8

1940-, Wilson John W., and Langley Research Center, eds. Radiation safety aspects of commercial high-speed flight transportation. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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9

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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10

Saltzman, Edwin J. Selected examples of NACA/NASA supersonic flight research. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Researh Center, 1995.

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11

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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12

Ayman, Kassem, and Langley Research Center, eds. Investigation of inner loop flight control strategies for high-speed. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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13

Ray, J. K. High-speed civil transport flight- and propulsion-control technological issues. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1992.

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14

Ray, J. K. High-speed civil transport flight- and propulsion-control technological issues. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1992.

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15

Aerodynamic principles of flight vehicles. Reston, VA: American Institute of Aeronautics and Astronautics, 2012.

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16

Reithmaier, L. W. Mach 1 and beyond: The illustrated guide to high-speed flight. New York: TAB Books, 1995.

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17

Ayman, Kassem, and Langley Research Center, eds. Investigation of inner loop flight control strategies for high-speed research. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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18

Bill, Gunston. Faster Than Sound: Story of Supersonic Flight. Sparkford, Somerset: P. Stephens, 1992.

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19

Kahlbaum, William M. High-speed real-time animated displays on the ADAGE RDS 3000 raster graphics system. Hampton, Va: Langley Research Center, 1989.

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20

L, Ownbey Katrina, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. High-speed real-time animated displays on the ADAGE® RDS 3000 Raster Graphics System. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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21

L, Ownbey Katrina, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. High-speed real-time animated displays on the ADAGE® RDS 3000 Raster Graphics System. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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22

Thompson, Milton O. Flight research: Problems encountered and what they should teach us. Washington, DC: NASA History Division, Office of Policy and Plans, NASA Headquarters, 2000.

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23

Center, Lewis Research, ed. Application of computational fluid dynamics in high speed aeropropulsion. [Cleveland, Ohio: Lewis Research Center, 1991.

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24

W, Jackson Dante, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. 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 Program, 1997.

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25

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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26

W, Jackson Dante, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. 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 Program, 1997.

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27

W, Jackson Dante, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, eds. 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 Program, 1997.

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28

T, Palmer Michael, and Langley Research Center, eds. A crew-centered flight deck design philosophy for high-speed civil transport (HSCT) aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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29

T, Palmer Michael, and Langley Research Center, eds. A Crew-centered flight deck design philosophy for high-speed civil transport (HSCT) aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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30

T, Palmer Michael, and Langley Research Center, eds. A Crew-centered flight deck design philosophy for high-speed civil transport (HSCT) aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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31

T, Palmer Michael, and Langley Research Center, eds. A Crew-centered flight deck design philosophy for high-speed civil transport (HSCT) aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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32

Wilson, J. W. Radiation safety issues in high altitude commercial aircraft. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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33

Taylor, Richard L. The first supersonic flight: Captain Charles E. Yeager breaks the sound barrier. New York: F. Watts, 1994.

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34

Center, Langley Research, ed. Initial piloted simulation evaluation of the Reference-H High-Speed Civil Transport design during takeoff and recovery from limit flight conditions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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35

Maung, Khin Maung. Radiation transport and shielding for space exploration and high speed flight transportation: Final report on NAG1-1789. [Washington, DC: National Aeronautics and Space Administration, 1997.

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36

Facility, Dryden Flight Research, ed. Monitoring techniques for the X-29A aircraft's high-speed rotating power takeoff shaft. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1990.

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37

United States. National Aeronautics and Space Administration., ed. Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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38

From kingfishers to ... bullet trains. Ann Arbor, Michigan: Cherry Lake Publishing, 2012.

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39

P, Gilbert William, Anglin Ernie L, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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40

R, McCarthy Thomas, and United States. National Aeronautics and Space Administration., eds. An integrated optimum design approach for high speed prop rotors: Final report on NASA Ames grant no. NCC2-795. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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41

W, Paulson John, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. A Review of technologies applicable to low-speed flight of high-performance aircraft investigated in the Langley 14- by 22-foot subsonic tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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42

W, Paulson John, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. A Review of technologies applicable to low-speed flight of high-performance aircraft investigated in the Langley 14- by 22-foot subsonic tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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43

G, Steenken W., and Hugh L. Dryden Flight Research Center., eds. Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

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44

Hallion, Richard. Supersonic flight: Breaking the sound barrier and beyond : the story of the Bell X-1 and Douglas D-558. London: Brassey's, 1997.

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45

K, Bogue Rodney, Seidel Jonathan, and Hugh L. Dryden Flight Research Center., eds. The use of a lidar forward-looking turbulence sensor for mixed-compression inlet unstart avoidance and gross weight reduction on a high speed civil transport. [Edwards, Calif.]: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

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46

A, McCurdy David, and Langley Research Center, eds. High-speed research: 1994 Sonic Boom Workshop : configuration design, analysis, and testing : proceedings of a workshop ... held in Hampton, Virginia, June 1-3, 1994. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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47

A, McCurdy David, and Langley Research Center, eds. High-speed research: 1994 Sonic Boom Workshop : configuration design, analysis, and testing : proceedings of a workshop ... held in Hampton, Virginia, June 1-3, 1994. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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48

A, McCurdy David, and Langley Research Center, eds. High-speed research: 1994 Sonic Boom Workshop : configuration design, analysis, and testing : proceedings of a workshop ... held in Hampton, Virginia, June 1-3, 1994. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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49

A, McCurdy David, and Langley Research Center, eds. High-speed research: 1994 Sonic Boom Workshop : configuration design, analysis, and testing : proceedings of a workshop ... held in Hampton, Virginia, June 1-3, 1994. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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50

A, McCurdy David, and Langley Research Center, eds. High-speed research: 1994 Sonic Boom Workshop : configuration design, analysis, and testing : proceedings of a workshop ... held in Hampton, Virginia, June 1-3, 1994. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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