Books on the topic 'Oblique wing'
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S, Alag Gurbux, Gilyard Glenn B, and Dryden Flight Research Facility, eds. Aeroelastic control of oblique-wing aircraft. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.
Find full textPhillips, James D. Modal control of an oblique wing aircraft. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.
Find full textKroo, Ilan. The aerodynamic design of oblique wing aircraft. American Institute of Aeronautics and Astronautics, 1986.
Find full textA, Kennelly Robert, and Ames Research Center, eds. Transonic wind tunnel test of a 14% thick oblique wing. National Aeronautics and Space Administration, Ames Research Center, 1990.
Find full textS, Alag Gurbux, and Dryden Flight Research Facility, eds. Model-following control for an oblique-wing aircraft. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.
Find full textS, Alag Gurbux, and Dryden Flight Research Facility, eds. Model-following control for an oblique-wing aircraft. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.
Find full textAlbert, Antaran, and United States. National Aeronautics and Space Administration., eds. RTJ-303: Variable geometry, oblique wing supersonic aircraft. National Aeronautics and Space Administration, 1992.
Find full textS, Alag Gurbux, and Dryden Flight Research Facility, eds. Model-following control for an oblique-wing aircraft. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.
Find full textAlbert, Antaran, and United States. National Aeronautics and Space Administration., eds. RTJ-303: Variable geometry, oblique wing supersonic aircraft. National Aeronautics and Space Administration, 1992.
Find full textW, Kempel Robert, Pahle Joseph W, and Dryden Flight Research Facility, eds. Decoupling control synthesis for an oblique-wing aircraft. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.
Find full textUnited States. National Aeronautics and Space Administration., ed. Design and testing of an oblique all-wing supersonic transport. MCAT Institute, 1994.
Find full textGreen, John A. Static aeroelastic analysis of a three-dimensional generic wing. National Aeronautics and Space Administration, Ames Research Center, 1990.
Find full textE, Curry Robert, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Flight characteristics of the AD-1 oblique-wing research aircraft. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Find full textFacility, Dryden Flight Research, ed. Output model-following control synthesis for an oblique-wing aircraft. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1990.
Find full textFacility, Dryden Flight Research, ed. Output model-following control synthesis for an oblique-wing aircraft. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1990.
Find full textFacility, Dryden Flight Research, ed. Output model-following control synthesis for an oblique-wing aircraft. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1990.
Find full textLarrimer, Bruce I. Thinking obliquely: Robert T. Jones, the Oblique Wing, NASA's AD-1 Demonstrator, and its legacy. NASA, 2013.
Find full textVincent, James H. Application of modern control design methodology to oblique wing research aircraft. Systems Control Technology, Inc., 1991.
Find full textKempel, Robert W. A piloted evaluation of an oblique-wing research aircraft motion simulation with decoupling control laws. Ames Research Center, 1988.
Find full textE, Curry Robert, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Flight-determined aerodynamic derivatives of the AD-1 oblique-wing research airplane. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Find full textE, Curry Robert, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Flight-determined aerodynamic derivatives of the AD-1 oblique-wing research airplane. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Find full textCenter, Ames Research, ed. The conceptual design of a Mach 2 oblique flying wing supersonic transport. National Aeronautics and Space Administration, Ames Research Center, 1989.
Find full textE, Curry Robert, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Flight-determined aerodynamic derivatives of the AD-1 oblique-wing research airplane. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Find full textE, Fortin Paul, and United States. National Aeronautics and Space Administration., eds. An integrated study of structures, aerodynamics, and controls on the forward swept wing X-29A and the oblique wing research aircraft. University of Kansas, Center for Research, 1987.
Find full textE, Fortin Paul, and United States. National Aeronautics and Space Administration, eds. An integrated study of structures, aerodynamics, and controls on the forward swept wing X-29A and the oblique wing research aircraft. University of Kansas, Center for Research, 1987.
Find full textCurry, Robert E. In-flight total forces, moments, and static aeroelestic characteristics of an oblique-wing research airplane. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Find full textCurry, Robert E. In-flight total forces, moments, and static aeroelestic characteristics of an oblique-wing research airplane. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Find full textCurry, Robert E. In-flight total forces, moments, and static aeroelestic characteristics of an oblique-wing research airplane. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Find full textMehta, Unmeel B. The computation of flow past an oblique wing using the thin-layer Navier-Stokes equations. National Aeronautics and Space Administration, Ames Research Center, 1988.
Find full textW, Kempel Robert, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. A piloted evaluation of an oblique-wing research aircraft motion simulation with decoupling control laws. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.
Find full textUnited States. National Aeronautics and Space Administration., ed. Design and testing of low sonic boom configurations and an oblique all-wing supersonic transport. MCAT Institute, 1995.
Find full textUnited States. National Aeronautics and Space Administration., ed. The leading edge 250: Oblique wing aircraft configuration project : final report 1987 - 88 : NASA/USRA advanced design program. California State Polytechnic University, Pomona Aerospace Engineering Dept., 1988.
Find full textUnited States. National Aeronautics and Space Administration, ed. Conceptual final paper on the preliminary design of an oblique flying wind SST. National Aeronautics and Space Administration, 1987.
Find full textB, Mehta Unmeel, and Ames Research Center, eds. Multiprocessing on supercomputers for computational aerodynamics. National Aeronautics and Space Administration, Ames Research Center, 1990.
Find full textHolland, Scott D. Mach 10 experimental database of a three-dimensional scramjet inlet flow field. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textCenter, Langley Research, ed. Mach 10 experimental database of a three-dimensional scramjet inlet flow field. National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textModel-following control for an oblique-wing aircraft. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.
Find full textRTJ-303: Variable geometry, oblique wing supersonic aircraft. National Aeronautics and Space Administration, 1992.
Find full textDesign and testing of an oblique all-wing supersonic transport. MCAT Institute, 1994.
Find full textFlight characteristics of the AD-1 oblique-wing research aircraft. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Find full textThe aerodynamic design of the oblique flying wing supersonic transport. Stanford University, 1990.
Find full textNational Aeronautics and Space Administration (NASA) Staff. Leading Edge 250: Oblique Wing Aircraft Configuration Project, Volume 4. Independently Published, 2018.
Find full textEigensystem synthesis for active flutter suppression on an oblique-wing aircraft. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.
Find full textSimplified aerodynamic and structural modeling for oblique all-wing aircraft--phase 2: structures: Final report for NASA NCA2-5025. National Aeronautics and Space Administration, 1994.
Find full textDesign and testing of low sonic boom configurations and an oblique all-wing supersonic transport. MCAT Institute, 1995.
Find full textDobson, Edward. Rudimentary Treatise on Masonry and Stonecutting: In Which the Principles of Masonic Projection and Their Application to the Construction of Curved Wing Walls, Domes, Oblique Bridges, and Roman and Gothic Vaulting Are Concisely Explained. Creative Media Partners, LLC, 2018.
Find full textRudimentary Treatise on Masonry and Stonecutting: In Which the Principles of Masonic Projection and Their Application to the Construction of Curved Wing Walls, Domes, Oblique Bridges, and Roman and Gothic Vaulting Are Concisely Explained. Creative Media Partners, LLC, 2023.
Find full textConceptual final paper on the preliminary design of an oblique flying wind SST. National Aeronautics and Space Administration, 1987.
Find full textEffects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle. National Aeronautics and Space Administration, Langley Research Center, 1999.
Find full textLi, Yinghong. Investigation on Oblique Shock Wave Control by Surface Arc Discharge in a Mach 2.2 Supersonic Wind Tunnel. INTECH Open Access Publisher, 2011.
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