Books on the topic 'Cambered wings'

Bolonkin, Alexander. Estimated benefits of variable-geometry wing camber control for transport aircraft. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

MacKinnon, A. Wind tunnel tests on a variable camber wing. Cranfield, Bedford, England: College of Aeronautics, Cranfield University, 1993.

Wood, Richard M. Study of lee-side flows over conically cambered delta wings at supersonic speeds. Hampton, Va: Langley Research Center, 1987.

Chu, Julio. Pressure meaurements on a thick cambered and twisted 58 [degree] delta wing at high subsonic speeds. Hampton, Va: Langley Research Center, 1987.

Wood, Richard M. Study of lee-side flows over conically cambered delta wings at supersonic speeds. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

Gilyard, Glenn B. In-flight transport performance optimization: An experimental flight research program and an operational scenario. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.

Gilyard, Glenn B. In-flight transport performance optimization: An experimental flight research program and an operational scenario. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.

Ashill, P. R. Control of leading-edge separation on a cambered delta wing. Farnborough: Defence Research Agency, 1993.

Smith, John W. Variable-camber systems integration and operational performance of the AFTI/F-111 mission adaptive wing. Edwards, California: NASA Dryden Flight Research Facility, 1992.

W, Smith John. Variable-camber systems integration and operational performance of the AFTI/F-111 mission adaptive wing. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1992.

W, Smith John. Variable-camber systems integration and operational performance of the AFTI/F-111 mission adaptive wing. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1992.

Smith, John W. Variable-camber systems integration and operational performance of the AFTI/F-111 mission adaptive wing. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1992.

Powers, Sheryll Goecke. Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

Powers, Sheryll Goecke. Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

Rudolph, Peter K. C. High-lift systems on commercial subsonic airliners. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1996.

Study of lee-side flows over conically cambered delta wings at supersonic speeds. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

B, Watson Carolyn, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. Study of lee-side flows over conically cambered delta wings at supersonic speeds. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

NASA Dryden Flight Research Center., ed. In-flight transport performance optimization: An experimental flight research program and an operational scenario. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.

NASA Dryden Flight Research Center., ed. In-flight transport performance optimization: An experimental flight research program and an operational scenario. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.

In-flight transport performance optimization: An experimental flight research program and an operational scenario. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.

Flight test of an adaptive configuration optimization system for transport aircraft. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

Flight test of an adaptive configuration optimization system for transport aircraft. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

Center, Langley Research, ed. Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

Facility, Dryden Flight Research, ed. A concept for adaptive performance optimization on commercial transport aircraft. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1995.

Center, Langley Research, and United States. National Aeronautics and Space Administration., eds. Euler technology assessment for preliminary aircraft design: Unstructured/structured grid NASTD application for aerodynamic analysis of an advanced fighter/tailless configuration. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

Pressure measurements on a thick cambered and twisted 58ʻ́. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

Gloria, Hernandez, and Langley Research Center, eds. Effect of leading- and trailing-edge flaps on clipped delta wings with and without wing camber at supersonic speeds. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Flight test results from a supercritical mission adaptive wing with smooth variable camber. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

Flow visualization study of a 1/48-scale AFTI/F111 model to investigate horizontal tail flow disturbances. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Facility, 1990.

Naomi, McMillin S., and Langley Research Center, eds. Surface-pressure and flow-visualization data at mach number 1.60 for three 65p0s delta wings varying in leading-edge radius and camber. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

Naomi, McMillin S., and United States. National Aeronautics and Space Administration., eds. Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camber. [Washington, D.C: National Aeronautics and Space Administration, 1996.

Naomi, McMillin S., and United States. National Aeronautics and Space Administration., eds. Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camber. [Washington, D.C: National Aeronautics and Space Administration, 1996.

Naomi, McMillin S., and United States. National Aeronautics and Space Administration., eds. Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camber. [Washington, D.C: National Aeronautics and Space Administration, 1996.

Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camber. [Washington, D.C: National Aeronautics and Space Administration, 1996.

Center, Ames Research, ed. High-lift systems on commercial subsonic airliners. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1996.

High-lift systems on commercial subsonic airliners. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1996.

Center, Ames Research, ed. High-lift systems on commercial subsonic airliners. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1996.

Center, Ames Research, ed. High-lift systems on commercial subsonic airliners. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1996.