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ItemThe long way to the tilt-rotor implementation( 1997) Renaud, J. ; Klein, J.M.
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ItemCarbon-epoxy laminated cylindrical shells under axial compression( 1997) Bisagni, C.
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ItemElementary study for the effect of HHC and active flap on blade vortex interaction( 1997) Kobiki, N. ; Tsuchihashi, A. ; Murashige, A. ; Yamakawa, E.
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ItemExperience with optimal input design for helicopter parameter identification( 1997) Sridhar, J.K. ; Place, C.S. ; Breeman, J.H.
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ItemThe status of human factor in civil rotorcraft safety( 1997) Hughes, T. ; Ingram, D.
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ItemPhenomenon of a coaxial helicopter high figure of merit at hover( 1997) Bourtsev, B.N. ; Kvokov, V.N. ; Vainsein, I.M. ; Petrosian, E.A.
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ItemBlade-tip vortex measurement by PIV( 1997) Murashige, A. ; Tsuchihashi, A. ; Tsujiuchi, T. ; Yamakawa, E.
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ItemEC135 structural testing( 1997) Barnersoi, H. ; Panajott, A. v. ; Pfeiffer, K. ; Vorwerg, R.
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ItemCoupling of aerodynamic and dynamic methods for the calculation of helicopter rotors in forward flight( 1997) Buchtala, B. ; Wehr, D. ; Wagner, S.
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ItemXV-15 aeroacoustic testing at NASA Ames( 1997) Light, J.S. ; Kitaplioglu, C. ; Acree, C.W.
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ItemSensor locations and active vibration control in helicopters( 1997) Venkatesan, C. ; Udayasankar, A.
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ItemDesign and test evaluation of FBR bearingless main rotor( 1997) Nakadate, M. ; Kawakami, N. ; Takaki, J.
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ItemPeriodic-coefficient finite-state aerodynamci modeling for rotor dynamics of helicopter configurations( 1997) De Troia, R. ; Gennaretti, M. ; Morino, L.
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ItemDynamic modelling and aeroelastic analysis of rotor system using CFD code & ADAMS package( 1997) Ahn, B.H. ; Lee, D.H.
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ItemA qualitative examination of dynamic stall from flight test data( 1997) Bousman, W.G.
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ItemNH90 TTH: The mission adaptable helicopter - The mission flight aids( 1997) Böhm, H.-D.V. ; Erismann, Ph.
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ItemThe lift deficiency matrix of a hovering helicopter rotor( 1997) Rosen, A.
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ItemThe TIGER development simulator( 1997) Karl, W.