Add to ORKGResults are presented from an investigation of the variation with Reynolds number and Mach number of the total, base, and skin-friction drag of seven boattail bodies of revolution designed for minimum wave drag according to the theory of NACA-TN-2550. The tests covered a Reynolds number range from approximately 1.0 x 10(6) to 10.0 x 10(6) at Mach numbers of 1.62, 1.93, and 2.41 respectively
Average skin-friction drag coefficients were obtained from boundary-layer total-pressure measurement...
An experimental investigation was conducted in the AEDC 16-foot Transonic Wind Tunnel (16T) to deter...
Report presenting an experimental investigation concerned primarily with the extension of test data ...
Results are presented from an investigation of the variation with Reynolds number and Mach number of...
An investigation has been conducted in the Langley 9-inch supersonic tunnel to determine the effect ...
Afterbody pressure distributions and wave drag were calculated using a second-order theory for a var...
The effects of fineness ratio (14.2 and 12.2) and boattailing on aerodynamic characteristics of four...
"December 1, 1953."Includes bibliographical references (p. 10).Mode of access: Internet
Average skin-friction drag coefficients were obtained from boundary-layer total-pressure measurement...
An experimental investigation was conducted in the AEDC 16-foot Transonic Wind Tunnel (16T) to deter...
Report presenting an experimental investigation concerned primarily with the extension of test data ...
Results are presented from an investigation of the variation with Reynolds number and Mach number of...
An investigation has been conducted in the Langley 9-inch supersonic tunnel to determine the effect ...
Afterbody pressure distributions and wave drag were calculated using a second-order theory for a var...
The effects of fineness ratio (14.2 and 12.2) and boattailing on aerodynamic characteristics of four...
"December 1, 1953."Includes bibliographical references (p. 10).Mode of access: Internet
Average skin-friction drag coefficients were obtained from boundary-layer total-pressure measurement...
An experimental investigation was conducted in the AEDC 16-foot Transonic Wind Tunnel (16T) to deter...
Report presenting an experimental investigation concerned primarily with the extension of test data ...