Books on the topic 'Blade flutter'
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United States. National Aeronautics and Space Administration., ed. Blade row interaction effects on flutter and forced response. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Find full textBlade row interaction effects on flutter and forced response. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Find full text1960-, Murthy Durbha V., and United States. National Aeronautics and Space Administration., eds. Aeroelastic modal characteristics of mistuned blade assemblies: Mode localization and loss of Eigenstructure. [Washington, DC]: National Aeronautics and Space Administration, 1991.
Find full textA 3D Theodorsen-Based Rotor Blade Flutter Model Using Normal Modes. Storming Media, 2002.
Find full textOral, Mehmed, and United States. National Aeronautics and Space Administration., eds. Optical measurement of unducted fan flutter. [Washington, DC]: NASA, 1991.
Find full textMethodology of blade unsteady pressure measurement in the NASA transonic flutter cascade. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.
Find full textV, Kaza K. R., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Analysis of an unswept propfan blade with a semiempirical dynamic stall model. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.
Find full textUnited States. National Aeronautics and Space Administration., ed. On curve veering and flutter of rotating blades. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Find full textUnited States. National Aeronautics and Space Administration., ed. On curve veering and flutter of rotating blades. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Find full textThe effect of steady aerodynamic loading on the flutter stability of turbomachinery blading. [Washington, DC]: National Aeronautics and Space Administration, 1991.
Find full textA, Simons Todd, and NASA Glenn Research Center, eds. Application of TURBO-AE to flutter prediction: Aeroelastic code development. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textA, Simons Todd, and NASA Glenn Research Center, eds. Application of TURBO-AE to flutter prediction: Aeroelastic code development. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textA, Simons Todd, and NASA Glenn Research Center, eds. Application of TURBO-AE to flutter prediction: Aeroelastic code development. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textV, Kaza K. R., and Lewis Research Center, eds. Experimental classical flutter results of a composite advanced turboprop model. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.
Find full textCenter, Lewis Research, ed. Mass balancing of hollow fan blades. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.
Find full textA Three-Dimensional Flutter Theory For Rotor Blades With Trailing-Edge Flaps. Storming Media, 2003.
Find full textRakesh, Srivastava, and United States. National Aeronautics and Space Administration., eds. Final technical report for Euler/Navier-Stokes solvers applied to ducted fan configurations: NASA grant number NAG3-1230 : grant duration, December 20, 1990 to December 20, 1996. [Washington, DC: National Aeronautics and Space Administration, 1997.
Find full textSanford, Fleeter, and Lewis Research Center, eds. The predicted effect of aerodynamic detuning of coupled bending-torsion unstalled supersonic flutter. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.
Find full textUnited States. National Aeronautics and Space Administration., ed. Unstalled flutter stability predictions and comparisions [sic] to test data for a composite prop-fan model. [Windsor Locks, CT]: Hamilton Standard Division, United Technologies Corp., 1986.
Find full textR, Srivastava, and United States. National Aeronautics and Space Administration., eds. User's guide for MSAP2D: A program for unsteady aerodynamic and aeroelastic (flutter and forced response) analysis of multistage compressors and turbines : under grant NAG3-1137. [Washington, DC: National Aeronautics and Space Administration, 1996.
Find full textJ, Usab William, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Application of a linearized unsteady aerodynamic analysis to standard cascade configurations. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Find full textCrosse, Gordon. Thel: Concertante for Solo Flute with Double String Septet and Two Horns After the Poem by William Blake: Op. 38 (Oxford Music for Trombone). Oxford University Press, 1989.
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