Books on the topic 'Supercritical Airfoil'

Maurice, Holt. Supercritical flow past a symmetrical bicircular arc airfoil. Berkeley, CA: Dept. of Mechanical Engineering, University of California, 1989.

Mokry, M. Influence of the transonic doublet in the farfield of a lifting airfoil. Ottawa: National Research Council Canada, Institute for Aerospace Research, 1993.

Jenkins, Renaldo. Aerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-Meter Transonic Cryogenic Tunnel. Hampton, Va: Langley Research Center, 1988.

Chan, Y. Y. Comparison of boundary layer trips of disk and grit types on airfoil performance at transonic speeds. Ottawa: National Aeronautical Establishment, National Research Council Canada, 1988.

Jenkins, Renaldo V. NASA SC(2)-0714 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-Meter Transonic Cryogenic Tunnel. Hampton, Va: Langley Research Center, 1989.

Khalid, M. Further studies on the 21% thick, supercritical NLR airfoil NAE 68-060-21:1. Ottawa: National Aeronautical Establishment, 1986.

Harris, Charles D. The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil: Design overview. Hampton, Va: Langley Research Center, 1988.

Lee, B. H. K. An experimental study of transonic buffet of a supercritical airfoil with trailing edge flap. Ottawa: National Research Council Canada, 1988.

Brooks, Cuyler W. The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil: Drag equations. Hampton, Va: Langley Research Center, 1989.

Chan, Y. Y. Analysis of experimental data for cast 10-2/DOA2 supercritical airfoil at high Reynolds numbers. Ottawa: National Research Council of Canada, 1988.

Brooks, Cuyler W. The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil: Suction coefficient analysis. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

Brooks, Cuyler W. The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil: Suction coefficient analysis. Hampton, Va: Langley Research Center, 1991.

Brooks, Cuyler W. The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil: Suction coefficient analysis. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

Brooks, Cuyler W. The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil: Suction coefficient analysis. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

Harris, Charles D. The NASA Langley laminar-flow-control experiment on a swept supercritical airfoil: Basic results for slotted configuration. Hampton, Va: Langley Research Center, 1989.

Harris, Charles D. The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil: Evaluation of initial perforated configuration. Hampton, Va: Langley Research Center, 1992.

Chan, Y. Y. Analysis of experimental data for cast 10-2/DOA 2 supercritical airfoil at low Reynolds numbers and application to high Reynolds number flow. Ottawa: National Research Council of Canada, 1989.

Harris, Charles D. NASA supercritical airfoils: a matrix of family-related airfoils. Hampton, Va: Langley Research Center, 1990.

Johnson, William G. Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Johnson, William G. Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Hirose, Naoki. Computational and experimental research on buffet phenomena of transonic airfoils. Tokyo: National Aerospace Laboratory, 1988.

Carlson, Leland A. A direct-inverse method for transonic and separated flows about airfoils. Hampton, Va: Langley Research Center, 1990.

Hirose, Naoki. Blunt trailing edge analysis of supercritical airfoils by a Navier-Stokes code. Tokyo, Japan: National Aerospace Laboratory, 1990.

Boer, R. G. den. Revised results of the unsteady transonic pressure measurements on the LANN model. Amsterdam: National Aerospace Laboratory, 1989.

Seidel, David A. Unsteady-pressure and dynamic-deflection measurements on an aeroelastic supercritical wing. Hampton, Va: Langley Research Center, 1991.

Badavi, Forooz F. Numerical simulation and comparison of symmetrical/supercritical airfoils for the near tip region of a helicopter in forward flight. Hampton, Va: Langley Research Center, 1989.

A, Wahls Richard, and Langley Research Center, eds. Comparison of computational and experimental results for a supercritical airfoil. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

W, Edwards John, and Langley Research Center, eds. Cryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. NASA SC(2)-0714 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. NASA SC(2)-0714 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. NASA SC(2)-0714 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

1934-, Harvey William D., Brooks Cuyler W, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil: Design overview. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

1934-, Harvey William D., Brooks Cuyler W, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil: Design overview. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil: Design overview. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

1952-, Harris Charles D., Harvey William D. 1934-, United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., and Langley Research Center, eds. The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil: Suction coefficient analysis. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

1952-, Harris Charles D., ed. The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil: Evaluation of initial perforated configuration. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1992.

1952-, Harris Charles D., ed. The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil: Evaluation of initial perforated configuration. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1992.

1952-, Harris Charles D., ed. The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil: Evaluation of initial perforated configuration. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1992.

1952-, Harris Charles D., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. The NASA Langley laminar-flow-control experiment on a swept supercritical airfoil: Basic results for slotted configuration. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

W, Hess R., and Langley Research Center, eds. Highlights of unsteady pressure tests on a 14 percent supercritical airfoil at high Reynolds number, transonic condition. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

The NASA Langley laminar-flow-control experiment on a swept supercritical airfoil: Basic results for slotted configuration. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Control of unsteady separated flow associated with the dynamic stall of airfoils. San Jose, CA: MCAT Institute, 1992.

United States. National Aeronautics and Space Administration., ed. Control of unsteady separated flow associated with the dynamic stall of airfoils: Final report, 95-09. San Jose, CA: MCAT Institute, 1995.

United States. National Aeronautics and Space Administration., ed. Control of unsteady separated flow associated with the dynamic stall of airfoils. San Jose, CA: MCAT Institute, 1994.

NASA supercritical airfoils: A matrix of family-related airfoils. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Ray, Dagenhart J., and Langley Research Center, eds. Two experimental supercritical laminar-flow-control swept-wing airfoils. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., ed. A direct-inverse method for transonic and separated flows about airfoils. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Office, 1990.

A direct-inverse method for transonic and separated flows about airfoils. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Office, 1990.

C, Sanford M., Eckstrom Clinton V, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, eds. Unsteady-pressure and dynamic-deflection measurements on an aeroelastic supercritical wing. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

C, Sandford M., Eckstrom Clinton V, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Unsteady-pressure and dynamic-deflection measurements on an aeroelastic supercritical wing. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.