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Structural model control and gust load alleviation for SensorCraft concept
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Austin, TX, April 18-21
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Shimko, T. and Vartio, E., "Structural Model Control And Gust Load Alleviation For SensorCraft Concept," 46th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, Austin, TX, April 18-21 2005.
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46th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference
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Shimko, T.1
Vartio, E.2
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2
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Static aeroelasticity and the flying wing
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October
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Weisshaar, T.A.1
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3
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Static aeroelasticity and the flying wing, revisited
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November
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Weisshaar, T. A. and Ashley, H., "Static Aeroelasticity and the Flying Wing, Revisited," Journal of Aircraft, Vol. 11, No. 11, November 1974, pp. 718-720.
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Weisshaar, T.A.1
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Die Geschichte der Horten-Flugzeuge 1933-1960
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Horten, R.1
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DVA, Stuttgart, Germany
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Fuchs, O., Gronau, W. V., and Sanger, E., Starten und Fliegen, Band V, DVA, Stuttgart, Germany, 1960.
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Fuchs, O.1
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7
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Handling and performance characteristics of swept-forward wing aircraft
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SAE-Paper 750548, Wichita, KS, April 8-11
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Marske, J. J., "Handling and Performance Characteristics of Swept-Forward Wing Aircraft," SAE-Paper 750548, Business Aircraft Meeting, Wichita, KS, April 8-11 1975.
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Business Aircraft Meeting
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Marske, J.J.1
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8
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Flutter characteristics of high aspect ratio tailless aircraft
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September
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Banerjee, J. R., "Flutter Characteristics of High Aspect Ratio Tailless Aircraft," Journal of Aircraft, Vol. 21, No. 9, September 1984, pp. 733-736.
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Banerjee, J.R.1
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Flutter analysis of a flying wing sensorcraft configuration using pre-stressed and rigid body frequencies and mode shapes
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AIAA 2005-2173, Austin, TX, April 18-21
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Strong, D., Kolonay, R., and Huttsell, L., "Flutter Analysis of a Flying Wing Sensorcraft Configuration Using Pre-Stressed and Rigid Body Frequencies and Mode Shapes," AIAA 2005-2173, 46th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, Austin, TX, April 18-21 2005.
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(2005)
46th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference
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Strong, D.1
Kolonay, R.2
Huttsell, L.3
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10
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28844440248
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Body freedom flutter of high aspect ratio flying wings
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AIAA 2005-1947, Austin, TX, April 18-21
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Nicoli, L., Lundgren, G., Zink, S., and Love, M., "Body Freedom Flutter of High Aspect Ratio Flying Wings," AIAA 2005-1947, 46th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, Austin, TX, April 18-21 2005.
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46th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference
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Nicoli, L.1
Lundgren, G.2
Zink, S.3
Love, M.4
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11
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0031682878
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Residual Pitch Oscillation (RPO) flight test and analysis on the B-2 bomber
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AIAA 98-1805, Long Beach, CA, April 20-23
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Jacobson, S. B., Britt, R. T., Dreim, D. R., and Kelly, P. D., "Residual Pitch Oscillation (RPO) Flight Test and Analysis on the B-2 Bomber," AIAA 98-1805, 39th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, Long Beach, CA, April 20-23 1998.
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(1998)
39th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference
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Jacobson, S.B.1
Britt, R.T.2
Dreim, D.R.3
Kelly, P.D.4
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12
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28844487094
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AIAA 2005-1944, 46th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, Austin, TX, April 18-21
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Beran, P. S., Hur, J., Snyder, R., Bryson, D., and Strganac, T., "Static Nonlinear Aeroelastic Analysis of a Blended-Wing Body," AIAA 2005-1944, 46th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, Austin, TX, April 18-21 2005.
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(2005)
Static Nonlinear Aeroelastic Analysis of a Blended-wing Body
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Beran, P.S.1
Hur, J.2
Snyder, R.3
Bryson, D.4
Strganac, T.5
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13
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The joined wing: An overview
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March
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3WoIkovitch, J., 'The Joined Wing: An Overview," Journal of Aircraft, Vol. 23, March 1986, pp. 161-178.
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Journal of Aircraft
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Woikovitch, J.1
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14
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0029710536
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Structural optimization for joind-wing synthesis
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January-February
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Journal of Aircraft
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Gallman, J.W.1
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15
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A joined-wing aeroelastic design with geometric non-linearity
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IFASD US-5, Amsterdam, TX, June 46
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Blair, M. and Canfield, R., "A Joined-Wing Aeroelastic Design With Geometric Non-linearity," IFASD US-5,International Forum on Aeroelasticity and Structural Dynamics, Amsterdam, TX, June 46 2003.
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International Forum on Aeroelasticity and Structural Dynamics
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Blair, M.1
Canfield, R.2
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16
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28844438781
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Static aeroelastic analysis of a high-altitude long-endurance joined-wing aircraft
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Austin, TX, April 18-21
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Snyder, R., Hur, J., Strong, D., and Beran, P. S., "Static Aeroelastic Analysis of a High-Altitude Long-Endurance Joined-Wing Aircraft," 46th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, Austin, TX, April 18-21 2005.
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(2005)
46th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference
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Snyder, R.1
Hur, J.2
Strong, D.3
Beran, P.S.4
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17
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28844455036
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The application of the MISTC framework to structural design application
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AIAA 2005-2127, Austin, TX, April 18-21
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Hunten, K., McCulley, C., Garza, A. D. L., and Blair, M., "The Application of the MISTC Framework to Structural Design Application," AIAA 2005-2127, 46th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, Austin, TX, April 18-21 2005.
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(2005)
46th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference
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Hunten, K.1
McCulley, C.2
Garza, A.D.L.3
Blair, M.4
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18
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85067318027
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Aeroelasticity of joined-wing airplane configurations: Past work and future challanges-A survey
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AIAA 2001-1370, Seattle, CWA, April 16-19
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Livne, E., "Aeroelasticity of Joined-Wing Airplane Configurations: Past Work and Future Challanges-A Survey," AIAA 2001-1370, 42nd AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, Seattle, CWA, April 16-19 2001.
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(2001)
42nd AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference
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Livne, E.1
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