论文信息 - Collection of zero-lift drag data on bodies of revolution from free-flight investigations

Collection of zero-lift drag data on bodies of revolution from free-flight investigations

Report presenting a compilation of most of the zero-lift drag obtained from free-flight measurements on fin-stabilized bodies of revolution. Results regarding friction drag, base pressure and base drag, pressures on a forward facing step, and fin pressure drag are provided.

William E Stoney | W. Stoney

[1] L. H. Jorgensen,et al. Investigation of the Drag of Various Axially Symmetric Nose Shapes of Fineness Ratio 3 for Mach Numbers from 1.24 to 7.4 , 1952 .

[2] W. Stoney. Transonic Drag Measurements of Eight Body-Nose Shapes , 1954 .

[3] Richard E Walters. Application of transonic area rule to a sharp-lipped ducted nacelle , 1954 .

[4] R. Sears,et al. Flight determination of drag of normal-shock nose inlets with various cowling profiles at Mach numbers from 0.9 to 1.5 , 1953 .

[5] R. Sears,et al. Flight determination of the drag and pressure recovery of an NACA 1-40-250 nose inlet at Mach numbers from 0.9 to 1.8 , 1955 .

[6] A. J. Eggers,et al. Bodies of revolution having minimum drag at high supersonic airspeeds , 1956 .

[7] R. G. Hart,et al. Flight Investigations at High-Subsonic, Transonic, and Supersonic Speeds to Determine Zero-Lift Drag of Fin-Stabilized Bodies of Revolution having Fineness Ratios of 12.5, 8.91, and 6.04 and Varying Positions of Maximum Diameter , 1949 .

[8] Robert O Piland,et al. Zero-lift drag of several conical and blunt nose shapes obtained in free flight at Mach numbers of 0.7 to 1.3 , 1956 .

[9] Eugene S. Love,et al. The Base Pressure at Supersonic Speeds on Two-Dimensional Airfoils and Bodies of Revolution (With and Without Fins) Having Turbulent Boundary Layers , 1953 .