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Volumn 5, Issue , 2003, Pages 3696-3706

Morphing wings of a small scale UAV using inflatable actuators: Sweep control

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AIRCRAFT; EQUIPMENT TESTING; FUSELAGES; INFLATABLE EQUIPMENT; MATHEMATICAL MODELS; MECHANICAL VARIABLES CONTROL; PERFORMANCE; UNMANNED VEHICLES; WIND TUNNELS;

EID: 0042009894     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (12)

References (18)
  • 1
    • 4243887358 scopus 로고
    • Wing plan forms for high-speed flight
    • NACA Report 863
    • Robert T. Jones, "Wing Plan Forms for High-Speed Flight," NACA Report 863. 1945
    • (1945)
    • Jones, R.T.1
  • 2
    • 0042722993 scopus 로고
    • Variable sweep: A case history of multiple re-innovation
    • the Rand Corporation, California
    • Robert L. Perry, "Variable Sweep: A Case History of Multiple Re-Innovation." the Rand Corporation, California. 1966
    • (1966)
    • Perry, R.L.1
  • 3
    • 0042722991 scopus 로고
    • The annals of the polymorph: A short history of variable geometry
    • April
    • "The Annals of the Polymorph: A Short history of Variable Geometry." Anonymous, Air International. April 1975
    • (1975) Anonymous, Air International
  • 4
    • 16244408089 scopus 로고
    • Variable sweep wing design
    • Grumman Aerospace Corporation. Bethpage, New York 11714
    • Robert W. Kress, "Variable Sweep Wing Design." Grumman Aerospace Corporation. Bethpage, New York 11714. 1983
    • (1983)
    • Kress, R.W.1
  • 5
    • 26144433847 scopus 로고
    • Flight testing of a variable sweep wing aircraft
    • AGARD-439, Paris, France
    • C. H. Meyer. "Flight Testing of a Variable Sweep Wing Aircraft." AGARD-439, Paris, France, 1963
    • (1963)
    • Meyer, C.H.1
  • 6
    • 26144451720 scopus 로고
    • Aerodynamic research relative to variable-sweep multimission aircraft
    • Langley Research Center, NASA N67-33072
    • Edward C. Polhamus and Alexander D. Hammond, "Aerodynamic Research Relative to Variable-Sweep Multimission Aircraft." Langley Research Center, NASA N67-33072. 1967
    • (1967)
    • Polhamus, E.C.1    Hammond, A.D.2
  • 7
    • 0043224228 scopus 로고
    • A theoretical study of the effect of pivot location on the aerodynamic-center movement of variable-sweep wings in incompressible flow
    • Langley Research Center, TN D-4635
    • John E. Lamar. "A Theoretical Study of the Effect of Pivot Location on the Aerodynamic-Center Movement of Variable-Sweep Wings in Incompressible Flow." Langley Research Center, TN D-4635, 1968
    • (1968)
    • Lamar, J.E.1
  • 8
    • 4244120536 scopus 로고    scopus 로고
    • Stability and control of flight vehicle
    • Lecture Notes, September
    • Uy-Loi Ly. "Stability and Control of Flight Vehicle," Lecture Notes, September 1997.
    • (1997)
    • Ly, U.-L.1
  • 9
    • 0003823386 scopus 로고
    • Dynamics of flight - Stability and control
    • John Wiley and Sons, Inc., New York
    • Bernard Etkin, "Dynamics of Flight - Stability and Control," John Wiley and Sons, Inc., New York, 1982
    • (1982)
    • Bernard, E.1
  • 10
    • 26144471959 scopus 로고
    • Effect of sweepback and aspect ratio on longitudinal stability characteristics of wings at low speeds
    • Langley Memorial Aeronautical Laboratory, NACA TN-1093
    • Joseph A. Shortal and Bernard Maggin, "Effect of Sweepback and Aspect Ratio on Longitudinal Stability Characteristics of Wings at Low Speeds." Langley Memorial Aeronautical Laboratory, NACA TN-1093, 1946
    • (1946)
    • Shortal, J.A.1    Maggin, B.2
  • 11
    • 26144465186 scopus 로고
    • Measurements of the damping in roll of large-scale swept-forward and swept-back wings
    • Ames Aeronautical Laboratory. NACA RM A7D11
    • Lynn W. Hunton and Joseph K. Dew, "Measurements of the Damping in Roll of Large-Scale Swept-Forward and Swept-Back Wings," Ames Aeronautical Laboratory. NACA RM A7D11. 1947
    • (1947)
    • Hunton, L.W.1    Dew, J.K.2
  • 12
    • 4243815844 scopus 로고
    • Note on the relative effect of the dihedral and the sweep back of airplane wings
    • NACA TN 177
    • Max M. Munk, "Note on the relative Effect of the Dihedral and the Sweep Back of Airplane Wings." NACA TN 177, 1924
    • (1924)
    • Munk, M.M.1
  • 13
    • 0003957909 scopus 로고    scopus 로고
    • Introduction to flight
    • McGraw-Hill
    • John D. Anderson Jr., "Introduction to Flight." McGraw-Hill. 1999
    • (1999)
    • Anderson J.D., Jr.1
  • 14
    • 0041721561 scopus 로고
    • A method for predicting lift increments due to flap deflection at low angles of attack in incompressible flow
    • Langley Aeronautical Laboratory, NACA TN3911
    • John G. Lowry, Edward C. Polhamus. "A Method for Predicting Lift Increments Due to Flap Deflection at Low Angeles of Attack in Incompressible Flow." Langley Aeronautical Laboratory, NACA TN3911. 1957
    • (1957)
    • Lowry, J.G.1    Polhamus, E.C.2
  • 15
  • 16
    • 0003631917 scopus 로고    scopus 로고
    • Aircraft design: A conceptual approach
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    • Daniel P. Raymer, "Aircraft Design: A Conceptual Approach", AIAA Education Series, 1999
    • (1999)
    • Raymer, D.P.1
  • 17
    • 0041721598 scopus 로고    scopus 로고
    • Prediction and verification of aerodynamic drag
    • Martin Summerfield Series Editor-in-chief
    • Charles E. Jobe. "Prediction and Verification of Aerodynamic Drag" in Progress in Astronautics and Aeronautics, vol. 98, Martin Summerfield Series Editor-in-chief
    • Progress in Astronautics and Aeronautics , vol.98
    • Jobe, C.E.1
  • 18
    • 0042221918 scopus 로고    scopus 로고
    • "Aircraft design synthesis and analysis." Version 1.0
    • Desktop Aeronautics. Inc.; January; via
    • Desktop Aeronautics. Inc., "Aircraft Design Synthesis and Analysis." Version 1.0. January 2003 via http://adg.stanford.edu/aa241
    • (2003)


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.