This report presents the first stage of an investigation of the response to random noise of a stiffened cylinder, representing an aircraft fuselage, including an analysis of the lower modes of such a cylinder. Preliminary ...
This report describes a series of free-flight tests designed to investigate various methods of body shaping to achieve low drag at transonic and supersonic speeds. In all, ten configurations were flown; three had unwaisted ...
Pressure and heat-transfer measurements have been made in free flight on a caret wing with blunt leading edges and nose, at speeds below and above the design Mach number of 2.47. Comparison with data from a corresponding ...
Pressure and heat-transfer measurements have been made on the lee surface of a delta wing at 14 degrees incidence in free flight over a Mach number range of 1.0 to 3.6 and at free-stream Reynolds numbers between 6 and 24 ...
Free-flight measurements have been made of the pressure distributions over a series of related afterbodies attached to a common cone-cylinder body of revohition. The Mach number range covered was from 0.9 to 1.5 and the ...
Measurements of the roll-damping derivative of three wing planforms were made by the free-flight roll-balance technique over the Mach number range 0.7 to 1.4. The wings were all of RAE 102 section, 7.5 per cent t/c and ...