Ballistic Limit of UHMWPE Composite Armor under Impact of Ogive-Nose ProjectileLi Ding, Xiaohui Gu, Peihui Shen & Xiangsheng KongPDF16 MB
Cavitation in Liquid Cryogens. IV, Combined Correlations for Venturi, Hydrofoil, Ogives, and PumpsJ. Hord1974
Computations of Supersonic Vortical Flows Around Ogive-cylinders Using Central and Upwind DifferencesEswar Josyula1997
Flow Visualization Photographs of a Yawed Tangent Ogive Cylinder at Mach Number 2 / J.H.Jones and J.E. O'Hare.J. Jones1973EN
Supersonic Flow Measurements in the Body Vortex Wake of an Ogive Nose Cylinder / W. L. Oberkampf, T. J. Bartel.William Oberkampf1978EN
Transonic Flow-field Calculation Around Ogive Cylinders by Nonlinear-linear Stretching Method / Jain-Ming Wu, Kinya Aoyama.Jain-Ming Wu1970EN
Force and Pressure Tests of Two Elliptic Ogive Body Shapes at Mach Numbers 5, 6, and 8Jack Burk1961EN
Vortex asymmetry development on a tangent ogive / William J. Yanta, Andrew B. Wardlaw, Jr., Daniel Sternklar.William Yanta1982EN
Calculation of Symmetric and Asymmetric Vortex Separation on Cones and Tangent Ogives Based on Discrete Vortex ModelsS. Chin1988EN
Investigation of boundary-layer suction on a 20-caliber Ogive cylinder at Mach numbers 2.5, 3.0, 3.5, and 4.0 / W.T. Strike and S. Pate.W. Strike1961EN
Support Interference on an Ogive-cylinder Model at High Angle of Attack in Transonic Flow / M.C. Altstatt and W.E. Dietz, Jr.M C Altstatt, W E Dietz & 4 more1978EN