Books on the topic 'Supersonic aircraft design'

Ramakrishnan, Sekaripuram. Supersonic flow computations for an ASTOVL aircraft configuration. Hampton, Va: Langley Research Center, 1990.

Boles, Michael A. Theoretical evaluation of engine auxiliary inlet design for supersonic V/STOL aircraft. Raleigh, N.C: Dept. of Mechanical and Aerospace Engineering, North Carolina State University, 1988.

Boles, Michael A. Theoretical evaluation of engine auxiliary inlet design for supersonic V/STOL aircraft. Raleigh, N.C: North Carolina State University, 1991.

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.

Fluid dynamics research on supersonic aircraft =: Les travaux de recherche en dynamique des fluides relatifs aux aéronefs supersoniques. [Neuilly-sur-Seine Cedex, France: North Atlantic Treaty Organization, Research and Technology Organization, 1998.

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.

Ardema, Mark D. Development of advanced methods of structural and trajectory analysis for transport aircraft: Annual report : October 1, 1995 - September 30, 1996. Santa Clara, CA: Santa Clara University, 1996.

Torenbeek, Egbert. Essentials of Supersonic Commercial Aircraft Conceptual Design. Wiley & Sons, Incorporated, John, 2020.

Essentials of Supersonic Commercial Aircraft Conceptual Design. Wiley & Sons, Limited, John, 2020.

Torenbeek, Egbert. Essentials of Supersonic Commercial Aircraft Conceptual Design. Wiley & Sons, Limited, John, 2020.

Torenbeek, Egbert. Essentials of Supersonic Commercial Aircraft Conceptual Design. Wiley & Sons, Incorporated, John, 2020.

Supersonic civil airplane study and design: Performance and sonic boom. San Jose, CA: MCAT Institute, 1995.

Aerodynamic Components of Aircraft at High Speeds. Princeton University Press, 2015.

Donovan, Allen F. Aerodynamic Components of Aircraft at High Speeds. Princeton University Press, 2016.

Donovan, Allen F. Aerodynamic Components of Aircraft at High Speeds. Princeton University Press, 2015.

J, Chattot J., Lawrence S. L, and United States. National Aeronautics and Space Administration., eds. Parallelization of a parabolized Navier-Stokes solver with a design optimizer: 34th AIAA Aerospace Sciences Meeting and Exhibit. [Washington, DC: National Aeronautics and Space Administration, 1996.

Center, NASA Glenn Research, ed. Conceptual design of a supersonic business jet propulsion system. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.

A, McGarry M., Reagan P. V, McDonnell Aircraft Company, and Lewis Research Center, eds. Research on a two-dimensional inlet for a supersonic V/STOL propulsion system. St. Louis, Mo.]: McDonnell Aircraft Company, McDonnell Douglas Corporation, 1989.

A, McGarry M., Reagan P. V, McDonnell Aircraft Company, and Lewis Research Center, eds. Research on a two-dimensional inlet for a supersonic V/STOL propulsion system. St. Louis, Mo.]: McDonnell Aircraft Company, McDonnell Douglas Corporation, 1989.

A, McGarry M., Reagan P. V, McDonnell Aircraft Company, and Lewis Research Center, eds. Research on a two-dimensional inlet for a supersonic V/STOL propulsion system. St. Louis, Mo.]: McDonnell Aircraft Company, McDonnell Douglas Corporation, 1989.

Evaluation of frameworks for HSCT design optimization. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

Evaluation of frameworks for HSCT design optimization. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

United States. National Aeronautics and Space Administration., ed. Design of a spanloader cargo aircraft: Final report, 1988-89. West Lafayette, Ind: Purdue University, 1989.

United States. National Aeronautics and Space Administration., ed. Design and testing of an oblique all-wing supersonic transport. San Jose, CA: MCAT Institute, 1994.

Design and testing of an oblique all-wing supersonic transport. San Jose, CA: MCAT Institute, 1994.

United States. National Aeronautics and Space Administration., ed. Advances in experiment design for high performance aircraft: Paper no. 8. [Washington, D.C: National Aeronautics and Space Administration, 1998.

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.

Preliminary design of a supersonic short takeoff and vertical landing (STOVL) fighter aircraft. [Washington, DC: National Aeronautics and Space Administration, 1990.

J, Maldonado Jaime, and Lewis Research Center, eds. Supersonic through-flow fan engine and aircrraft mission performance. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1989.

R, Chakravarthy Sukumar, Szema Kuo-Yen, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., and Langley Research Center, eds. Supersonic flow computations for an ASTOVL aircraft configuration: Phase 2, part 2. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1990.

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

Oktay, Baysal, and United States. National Aeronautics and Space Administration., eds. Three-dimensional aerodynamic shape optimization of supersonic delta wings: [abstract]. Washington, D.C: American Institute of Aeronautics and Astornautics, 1994.

Oktay, Baysal, and United States. National Aeronautics and Space Administration., eds. Three-dimensional aerodynamic shape optimization of supersonic delta wings: [abstract]. Washington, D.C: American Institute of Aeronautics and Astornautics, 1994.

A methodology for designing aircraft to low sonic boom constraints. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

Full potential methods for analysis/design of complex aerospace configurations. Los Angeles, Calif: Rockwell International Corp., 1986.

Center, Langley Research, and United States. National Aeronautics and Space Administration., eds. Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

1934-, Jameson Antony, and Research Institute for Advanced Computer Science (U.S.), eds. Supersonic wing and wing-body shape optimization using an adjoint formulation. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1995.

1934-, Jameson Antony, and Research Institute for Advanced Computer Science (U.S.), eds. Supersonic wing and wing-body shape optimization using an adjoint formulation. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1995.

1934-, Jameson Antony, and Research Institute for Advanced Computer Science (U.S.), eds. Supersonic wing and wing-body shape optimization using an adjoint formulation. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1995.

Caygill, Peter. Lightning Eject: The Dubious Safety Record of Britain's Only Supersonic Fighter. Pen & Sword Books Limited, 2013.

Caygill, Peter. Lightning Eject: The Dubious Safety Record of Britain's Only Supersonic Fighter. Pen & Sword Books Limited, 2013.

Caygill, Peter. Lightning Eject: The Dubious Safety Record of Britain's Only Supersonic Fighter. Pen & Sword Books Limited, 2013.

N, Tiwari S., and United States. National Aeronautics and Space Administration., eds. Aerodynamic shape optimization of a HSCT type configuration with improved surface definition: Progress report for the period ended June 30, 1994. Norfolk, VA: Old Dominion University Research Foundation, 1994.

Facility, Dryden Flight Research, ed. The design and use of a temperature-compensated hot-film anemometer system for boundary-layer flow transition detection on supersonic aircraft. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1988.

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.

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.

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.

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.

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.

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.