Books on the topic 'Angles of Euler'
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Nallasamy, M. Unsteady Euler analysis of the flow field of a propfan at an angle of attack. Lewis Research Center, 1990.
Find full textLessard, Wendy B. Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code. National Aeronautics and Space Administration, Langley Research Center, 1996.
Find full textLandis, Markley F., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Minimal parameter solution of the orthogonal matrix differential equation. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Find full textComparison of Quaternion and Euler Angle Methods for Joint Angle Animation of Human Figure Models. Storming Media, 1999.
Find full textF, Groeneweg John, and United States. National Aeronautics and Space Administration., eds. Unsteady Euler analysis of the flow field of a propfan at the angle of attack. National Aeronautics and Space Administration, 1990.
Find full textUnited States. National Aeronautics and Space Administration., ed. Euler/Navier-Stokes flow computations on flexible configurations for stability analysis. National Aeronautics and Space Administration, American Institute of Aeronautics and Astronautics, 1995.
Find full textUnited States. National Aeronautics and Space Administration., ed. Euler/Navier-Stokes flow computations on flexible configurations for stability analysis. National Aeronautics and Space Administration, American Institute of Aeronautics and Astronautics, 1995.
Find full textUnited States. National Aeronautics and Space Administration., ed. Euler/Navier-Stokes flow computations on flexible configurations for stability analysis. National Aeronautics and Space Administration, American Institute of Aeronautics and Astronautics, 1995.
Find full textEuler/Navier-Stokes flow computations on flexible configurations for stability analysis. National Aeronautics and Space Administration, American Institute of Aeronautics and Astronautics, 1995.
Find full textCenter, Langley Research, ed. Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code. National Aeronautics and Space Administration, Langley Research Center, 1996.
Find full textCenter, Langley Research, ed. Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code. National Aeronautics and Space Administration, Langley Research Center, 1996.
Find full textCenter, Langley Research, ed. Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code. National Aeronautics and Space Administration, Langley Research Center, 1996.
Find full textCenter, Langley Research, ed. Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code. National Aeronautics and Space Administration, Langley Research Center, 1996.
Find full textG, Podboy Gary, and United States. National Aeronautics and Space Administration., eds. Effects of a forward-swept front rotor on the flowfield of a counterrotation propeller. National Aeronautics and Space Administration, 1994.
Find full textG, Podboy Gary, and United States. National Aeronautics and Space Administration., eds. Effects of a forward-swept front rotor on the flowfield of a counterrotation propeller. National Aeronautics and Space Administration, 1994.
Find full textG, Podboy Gary, and United States. National Aeronautics and Space Administration., eds. Effects of a forward-swept front rotor on the flowfield of a counterrotation propeller. National Aeronautics and Space Administration, 1994.
Find full textCenter, Langley Research, ed. Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds. National Aeronautics and Space Administration, Langley Research Center, 1988.
Find full textCenter, Langley Research, and United States. National Aeronautics and Space Administration., eds. Euler technology assessment: SPLITFLOW code applications for stability and control analysis on an advanced fighter model employing innovative control concepts. National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textW, Harris Brenda, Raj Pradeep 1949-, and Langley Research Center, eds. An assessment of viscous effects in computational simulation of benign and burst vortex flows on generic fighter wind-tunnel models using TEAM code. National Aeronautics and Space Administration, Langley Research Center, 1995.
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