AN INVESTIGATION OF MODIFIED CLUSTERED JET-EXIT ARRANGEMENTS AT SUPERSONIC SPEEDS
Modified clustered jet-exit arrangements at supersonic speeds
CLUSTER↗
Engineering topics
Swihart, J. M.
Publications and source records attributed to Swihart, J. M..
Effect of Terminal Fairings on the Performance of a Plug-type Exhaust Nozzle in Quiescent Air and at Mach Numbers of 1.62, 1.93, 2.55, and 3.05
Explore the source record for details and available documents.
Norton, H. T., Jr.↗
Effect of Several Afterbody Modifications Including Terminal Fairings on the Drag of a Single-engine Fighter Model with Hot-jet Exhaust
Wind tunnel study of drag characteristics of boattailed afterbodies and afterbody terminal fairings for single engine jet aircraft
DRAG EFFECT↗
Performance of multiple jet-exit installations
Internal aerodynamics and performance of clustered jet-exit installations at transonic speeds
JET EXHAUST↗
Performance of multiple jet-exit installations
Explore the source record for details and available documents.
Nelson, W. J.↗
Transonic Aerodynamic Characteristics of a 1/15-Scale Model of the Convair B-58 Airplane
Explore the source record for details and available documents.
Swihart, J. M.↗
Transonic Aerodynamic and Trim Characteristics of a Multi-engine Delta-wing Airplane Model
Wind tunnel testing of two and four engine models of delta wing aircraft for transonic drag rise increment and maximum lift-drag ratio comparison
DRAG↗