Książki na temat „High speed flight”

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

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

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

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.

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

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

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

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

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.

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

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.

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

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.

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.

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

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

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

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

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

L, Ownbey Katrina, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. 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.

L, Ownbey Katrina, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. 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.

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.

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

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

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.

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

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

T, Palmer Michael, i Langley Research Center, red. 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.

T, Palmer Michael, i Langley Research Center, red. 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.

T, Palmer Michael, i Langley Research Center, red. 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.

T, Palmer Michael, i Langley Research Center, red. 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.

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

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

Center, Langley Research, red. 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.

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.

Facility, Dryden Flight Research, red. 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.

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

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

P, Gilbert William, Anglin Ernie L i United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. 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.

R, McCarthy Thomas, i United States. National Aeronautics and Space Administration., red. 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.

W, Paulson John, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. 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.

W, Paulson John, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. 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.

G, Steenken W., i Hugh L. Dryden Flight Research Center., red. 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.

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.

K, Bogue Rodney, Seidel Jonathan i Hugh L. Dryden Flight Research Center., red. 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.

A, McCurdy David, i Langley Research Center, red. 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.

A, McCurdy David, i Langley Research Center, red. 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.

A, McCurdy David, i Langley Research Center, red. 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.

A, McCurdy David, i Langley Research Center, red. 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.

A, McCurdy David, i Langley Research Center, red. 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.