Books on the topic 'Active aerodynamics'

Paduano, James D. Active control of rotating stall in axial compressors. Cambridge, Mass: Gas Turbine Laboratory, Massachusetts Institute of Technology, 1992.

Nissim, E. Control surface spanwise placement in active flutter suppression systems. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

Haynes, Joel M. Active control of rotating stall in a three-stage axial compressor. Cambridge, Mass: Gas Turbine Laboratory, Massachusetts Institute of Technology, 1993.

Nissim, E. Effect of control surface mass unbalance on the stability of a closed-loop active control system. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Ravindran, S. S. Active control of flow separation over an airfoil. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Ravindran, S. S. Active control of flow separation over an airfoil. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Li, Feng-Chen. Turbulent drag reduction by surfactant additives. Hoboken, N.J: Wiley, 2011.

Schwartz, Heather E. The science of a race car: Reactions in action. Mankato, Minn: Capstone Press, 2010.

Schwartz, Heather E. The science of a race car: Reactions in action. Mankato, Minn: Capstone Press, 2010.

S, Pototzky Anthony, and Langley Research Center, eds. Rolling maneuver load alleviation using active controls. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

S, Pototzky Anthony, and Langley Research Center, eds. Rolling maneuver load alleviation using active controls. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

R, Waszak Martin, and Langley Research Center, eds. Active flutter suppression using "dipole" filters. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

S, Liebst Bradley, Farm Jerome A, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. Eigenspace techniques for active flutter suppression. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

Gu, Zhongquan, Demao Zhu, and United States. National Aeronautics and Space Administration., eds. Investigation of control law for active flutter suppression. Washington, DC: National Aeronautics and Space Administration, 1988.

F, Badavi F., Noonan Kevin W, and Langley Research Center, eds. An application of active surface heating for augmenting lift and reducing drag of an airfoil. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

Eigensystem synthesis for active flutter suppression on an oblique-wing aircraft. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.

Boyd, Perry, Noll Thomas E, and Langley Research Center, eds. Flutter suppression control law synthesis for the active flexible wing model. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

M, Miller Jonathan, Doggett Robert V, and Langley Research Center, eds. Attenuation of empennage buffet response through active control of damping using piezoelectric material. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

S, Srinathkumar, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Design and experimental validation of a flutter suppression controller for the active flexible wing. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

T, Batina John, and Langley Research Center, eds. Conical Euler simulation and active suppression of delta wing rocking motion. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

United States. National Aeronautics and Space Administration., ed. A determination of the external forces required to move the benchmark active controls testing model in pure plunge and pure pitch. [Washington, DC]: National Aeronautics and Space Administration, 1993.

United States. National Aeronautics and Space Administration., ed. A determination of the external forces required to move the benchmark active controls testing model in pure plunge and pure pitch. [Washington, DC]: National Aeronautics and Space Administration, 1993.

M, Verdon Joseph, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Active control of wake/blade-row interaction noise through the use of blade surface actuators. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

T, Batina John, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Conical Euler analysis and active roll suppression for unsteady vortical flows about rolling delta wings. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Conical Euler analysis and active roll suppression for unsteady vortical flows about rolling delta wings. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Chithrabhanu, Koodalattupuram, Langley Research Center, Old Dominion University. Research Foundation, and Old Dominion University. School of Engineering, eds. An investigation of the feasibility of active boundary layer thickening for aircraft drag reduction. Norfolk, Va: Dept. of Mechanical Engineering and Mechanics, School of Engineering, Old Dominion University, 1986.

Biewener, Andrew A., and Shelia N. Patek, eds. Movement in Air. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198743156.003.0006.

Blade-mounted flap control for BVI noise reduction proof-of-concept test. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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.

Center, NASA Glenn Research, ed. Active control of fan noise by vane actuators. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

Center, NASA Glenn Research, ed. Active control of fan noise by vane actuators. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

Active load control during rolling maneuvers. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Jimmy, Fung, and Langley Research Center, eds. Parameter estimation of actuators for Benchmark Active Control Technology (BACT) wind tunnel model with analysis of wear and aerodynamic loading effects. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

Actuator feasibility study for active control of ducted axial fan noise: Under contract NAS3-26618. [Washington, DC: National Aeronautics and Space Administration, 1994.

Actuator feasibility study for active control of ducted axial fan noise: Under contract NAS3-26618. [Washington, DC: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. Analysis of the leading edge effects on the boundary layer transition: Technical report, March 1, 1984 - August 31, 1990. [Washington, DC: National Aeronautics and Space Administration, 1990.

Numerical simulation of the SOFIA flow field. San Jose, CA: MCAT Institute, 1995.

United States. National Aeronautics and Space Administration., ed. Numerical simulation of the SOFIA flowfield. San Jose, CA: MCAT Institute, 1994.

United States. National Aeronautics and Space Administration., ed. Numerical simulation of the SOFIA flowfield. San Jose, CA: MCAT Institute, 1994.

United States. National Aeronautics and Space Administration., ed. Numerical simulation of the SOFIA flowfield. San Jose, CA: MCAT Institute, 1994.

United States. National Aeronautics and Space Administration., ed. Numerical simulation of the SOFIA flow field. San Jose, CA: MCAT Institute, 1995.