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| Srl | Item |
| 1 |
ID:
164979
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| Summary/Abstract |
This article presents drag performance as a queer method of critique in the field of IR, which contributes to a longstanding move in IR to engage with aesthetics, and a more recent move to engage with performance art. The article discusses the author’s making of a performance piece that revisited the EU’s response to Hamas’s success in the 2006 Palestinian legislative elections. Soft, camp, feminine, and childlike voices; a female body in men’s clothing; and the translocation of bodies in spaces are used in the performance piece to disrupt the coherency of normalised diplomacy. Queer IR theory emphasises the imperative to dismantle logics of normality that prevent creativity in response to political issues. Performative drag practices disrupt anxious attachments to a ritualised discourse of strategic interests that shapes political initiatives. This article comments on other drag moments in politics, such as the anxiety around Jeremy Corbyn’s dress, Barack Obama’s anger translator, and Janelle Monáe’s androgynous articulation of community. The form that research dissemination takes implicates the kind of knowledge that is produced. This article reviews three methodological provocations of drag, an alternative departure point of the ‘what if’, performing a politics of refusal, and a Brechtian technique of estrangement.
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| 2 |
ID:
136039
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| Summary/Abstract |
Flow around a conical nose with rounded tail projectile has been studied numerically for subsonic, transonic and supersonic flow regimes. The conic angle of the projectile is 10°. The inflow Mach numbers are 0.5, 0.9, and 1.5. Axisymmetric Euler’s equations are solved for predicting the drag coefficient. It has been observed that even for a subsonic flow regime, the Mach number distribution is not uniform owing to the non-symmetric shape of the projectile. The predicted drag coefficients for subsonic, transonic, and supersonic cases are 0.018, 0.089, and 0.395, respectively. It was observed that rounded tail is a better option than boat tail so far drag force is concerned.
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