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Showing results 1 to 16 of 16
Issue DateTitleAuthor(s)
Mar-1995 Aerodynamic evaluation of production fuzes and fins for the 81 mm improved mortar projectilePierens, D.A.
Feb-1977 Calculation of pressure distributions on two axisymmetric boattailed configurationsHaselgrove, M.K.
Aug-1994 Data acquisition and processing software for the low speed wind tunnel tests of the Jindivik auxiliary air intakeLam, S.W.
Feb-1997 Effect of the leading-edge extension (LEX) fence on the vortex structure over the F/A-18Thompson, D.H.
Aug-1994 FFG-7 class frigate airwake viewerHeinze, C.A.; Arney, A.M.
Jan-1982 Flight tests of various MK82 bomb configurations.Dudley, R.E.; Pope, R.L.
Nov-2005 ImPressOne: a pressure display and acquisitions program for the low speed wind tunnel at DSTOBlandford, A
Feb-1999 MicroVAX/Bus communication testing software for the low speed wind tunnel data acquisition systemEdwards, C.D.
Jul-2012 Phase 1 Experimental Testing of a Generic Submarine Model in the DSTO Low Speed Wind Tunnel.Quick, H.; Widjaja, R.; Anderson, B., et al
Mar-2014 Phase II Experimental Testing of a Generic Submarine Model in the DSTO Low Speed Tunnel.Quick, H.; Woodyatt, B.
May-1994 Pitch and roll damping coefficients of the Australian 81mm improved mortar projectilePierens, D.A.
May-1994 A preliminary study of the airwake model used in an existing SH-60B/FFG-7 helicopter/ship simulation programErm, L.P.
May-1981 The use of a deflectable nose on a missile as a control device.Thomson, K.D.
Jul-2004 Wind tunnel simulations of the mock urban setting test : experimental procedures and data analysisGailis, R.
Sep-1979 Wind tunnel tests of a spinning 105 mm artillery shell model with canard control surfaces.Jermey, C.
Aug-1983 Wind tunnel tests on a tube-launched missile configuration with a deflectable nose control and a novel wrap-around fin stabiliser.Thomson, K.D.
Showing results 1 to 16 of 16


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