It’s not all about the music:online fan communities and collecting Hard Rock Café pins

Previous studies of music fan culture have largely centered on the diverse range of subcultures devoted to particular genres, groups, and stars. Where studies have moved beyond the actual music and examined the fashion, concerts, and collecting ephemera such as vinyl records and posters, they have tended to remain closely allied to notions of subcultural distinction, emphasizing hierarchies of taste. This paper shifts the focus in music fan studies beyond the appreciation of the music and discusses the popular fan practice of collecting souvenir pins produced and sold by the Hard Rock Café (HRC) within a framework of fan tourism. Traveling to and collecting unique pins from locations across the globe creates a fan dialogue that centers on tourism and the collecting practices associated with souvenir consumption. Collectors engage in practices such as blogging, travel writing, and administration that become important indicators of their particular expression of fandom: pin collecting. Membership requires both time and money; recording visits around the world and collecting unique pins from every café builds fans' cultural capital. This indicates an internationalization of popular fandom, with the Internet acting as a connective virtual space between local and national, personal and public physical space. The study of HRC pin collecting and its fan community suggests that HRC enthusiasts are not so because they enjoy rock music or follow any particular artist but due to the physical ephemera that they collect and the places and spaces they visit

Variable pitch fan system for NASA/Navy research and technology aircraft

Preliminary design of a shaft driven, variable-pitch lift fan and lift-cruise fan was conducted for a V/STOL Research and Technology Aircraft. The lift fan and lift-cruise fan employed a common rotor of 157.5 cm diameter, 1.18 pressure ratio variable-pitch fan designed to operate at a rotor-tip speed of 284 mps. Fan performance maps were prepared and detailed aerodynamic characteristics were established. Cost/weight/risk trade studies were conducted for the blade and fan case. Structural sizing was conducted for major components and weights determined for both the lift and lift-cruise fans

Generalised models for torsional spine and fan magnetic reconnection

Three-dimensional null points are present in abundance in the solar corona, and the same is likely to be true in other astrophysical environments. Recent studies suggest that reconnection at such 3D nulls may play an important role in the coronal dynamics. In this paper the properties of the torsional spine and torsional fan modes of magnetic reconnection at 3D nulls are investigated. New analytical models are developed, which for the first time include a current layer that is spatially localised around the null, extending along either the spine or the fan of the null. These are complemented with numerical simulations. The principal aim is to investigate the effect of varying the degree of asymmetry of the null point magnetic field on the resulting reconnection process - where previous studies always considered a non-generic radially symmetric null. The geometry of the current layers within which torsional spine and torsional fan reconnection occur is found to be strongly dependent on the symmetry of the magnetic field. Torsional spine reconnection still occurs in a narrow tube around the spine, but with elliptical cross-section when the fan eigenvalues are different, and with the short axis of the ellipse being along the strong field direction. The spatiotemporal peak current, and the peak reconnection rate attained, are found not to depend strongly on the degree of asymmetry. For torsional fan reconnection, the reconnection occurs in a planar disk in the fan surface, which is again elliptical when the symmetry of the magnetic field is broken. The short axis of the ellipse is along the weak field direction, with the current being peaked in these weak field regions. The peak current and peak reconnection rate in this case are clearly dependent on the asymmetry, with the peak current increasing but the reconnection rate decreasing as the degree of asymmetry is increased

Jane Austen fan fiction and the situated fantext: the example of Pamela Aidan's Fitzwilliam darcy, gentleman

Building on recent findings in the field of fan fiction studies, I claim that Pamela Aidan’s Fitzwilliam Darcy, Gentleman is indirectly influenced by three cultural phenomena which centre around Jane Austen and her work. Aidan’s fan fiction text stays close to the spirit of Austen’s Pride and Prejudice because she “reimagines” the novel according to the interpretive conventions of the Republic of Pemberley, a fan community. These conventions demand respect for Austen and her novels because they are shaped by the broader, cultural conventions of Janeitism and Austen criticism. Similarly, Aidan’s text is more individualistic and “Harlequinesque” than Austen’s novel, because the Republic allows writers to reproduce the cultural reading which underlies BBC / A&E’s adaptation of Austen’s novel

NASA/Navy lift/cruise fan cost reduction studies

Cost reduction studies were performed for the LCF459 turbotip fan for application with the YJ97-GE-100 gas generator in a multimission V/STOL research and technology aircraft. A 20 percent cost reduction of the research configuration based on the original preliminary design was achieved. The trade studies performed and the results in the area of cost reduction and weight are covered. A fan configuration is defined for continuation of the program through the detailed design phase

Experimental and theoretical studies of subsonic fan noise

The noise generated by inlet turbulence impinging on a subsonic axial flow fan was studied as a function of tip speed, flow coefficient, and intensity and scale of turbulence was carried out. Both turbulence and far field acoustic measurements were made. The new elements introduced in the theoretical analysis were accounting for blade loading dependent noise mechanisms and consideration of anisotropic turbulence impinging on the rotor because of inlet flow contraction effects. Experimentally an unexplained increase of noise at about 1/2 and 1 1/2 times blade passsing frequency was observed at low flow coefficients even though there was no evidence of compressor surge. In the final version the theory does a fair job of predicting variations of noise with blade loading and tip speed. Alteration of inlet turbulence length scales produced some but not very pronounced changes in the far field PWL spectra. Some degree of eddy contraction and resulting anisotropy were essential to explain the concentration of energy around blade passing frequencies

A preliminary design study of supersonic through-flow fan inlets

From Mach 3.20 cruise propulsion systems, preliminary design studies for two supersonic through-flow fan primary inlets and a single core inlet were undertaken. Method of characteristics and one dimensional performance techniques were applied to assess the potential improvements supersonic through-flow fan technology has over more conventional systems. A fixed geometry supersonic through-flow fan primary inlet was found to have better performance than a conventional inlet design on the basis of total pressure recovery, air flow, aerodynamic drag and size and weight

Experimental and analytical dynamic flow characteristics of an axial-flow fan from an air cushion landing system model

An investigation was conducted to compare the steady-state and dynamic flow characteristics of an axial-flow fan which had been used previously as the air supply fan for some model air cushion landing system studies. Steady-state flow characteristics were determined in the standard manner by using differential orifice pressures for the flow regime from free flow to zero flow. In this same regime, a correlative technique was established so that fan inlet and outlet pressures could be used to measure dynamic flow as created by a rotating damper. Dynamic tests at damper frequencies up to 5 Hz showed very different flow characteristics when compared with steady-state flow, particularly with respect to peak pressures and the pressure-flow relationship at fan stall and unstall. A generalized, rational mathematical fan model was developed based on physical fan parameters and a steady-state flow characteristic. The model showed good correlation with experimental tests at damper frequencies up to 5 Hz

The supersonic fan engine: An advanced concept in supersonic cruise propulsion

Engine performance and mission studies were carried out for turbofan engines equipped with supersonic through-flow fans. The mission was for a commercial supersonic transport with a Mach 2.32 capability. The advantages of the supersonic fan engines are discussed in terms of mission range comparisons with other engine types. The effects of fan efficiency, inlet losses, and engine weight on engine performance and mission range are shown. The range of a supersonic transport with supersonic fan engines could be 10 to 20 percent better than with other types having the same technology core