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41
Oscillating supersonic delta wings with curved leading edges
Published 2010“…In the present study Supersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing for the attached shock case. A strip theory is used in which strips at different span-wise locations are independent. …”
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Article -
42
Effect of angle of incidence on stability derivatives of a wing
Published 2014“…In the Present paper effect of angle of incidence on pitching derivatives of a delta wing with curved leading edges of a attached shock case is been studied. …”
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Article -
43
Oscillating supersonic delta wing with straight leading edges
Published 2012“…A Supersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing with straight leading edge for the attached shock case. …”
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Article -
44
Oscillating supersonic delta wings with straight leading edges
Published 2012“…A Supersonic similitude has been used to obtain stability derivatives in pitch and roll of a delta wing with straight leading edge for the attached shock case. …”
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Article -
45
Evaluation of aircraft wing-tip vortex using PIV
Published 2009“…The formation and development of a wing-tip vortex in a near and extended near filed were studied experimentally. …”
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Proceeding Paper -
46
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47
Printing fine solid lines in flexographic printing process
Published 2011“…The experiments also point the importance of light engagement pressures within the printing train and the requirements for using anilox cylinders having fine engraving. The work also shows than process parameters (eg, contact pressures) that are important for graphics printing have a similar effect when the processes is used to print fine line features . .…”
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Thesis -
48
The properties of concrete containing coconut shell as fine aggregate
Published 2020“…In terms of mechanical properties, concrete containing fine coconut shell as a partial replacement of fine aggregate demonstrated better performance than normal concrete. …”
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Thesis -
49
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50
Long memory in the Ukrainian stock market
Published 2013“…This paper examines the dynamics of stock prices in Ukraine by estimating the degree of persistence of the PFTS stock market index. Using long memory techniques we show that the log prices series is I(d) with d slightly above 1, implying that returns are characterised by a small degree of long memory and thus are predictable using historical data. …”
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Article -
51
Letter to Mr J J Long
Published 1939“…Typescript letter asking if Mr Long can speak at the upcoming meeting on 28 March and updating him on other developments. …”
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Correspondence -
52
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53
Letter from J. J. Long
Published 1939“…Typescript letter dated 21 April 1939, addressed "Dear Tom", from J J Long, about a meeting of the branch.…”
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Correspondence -
54
Frequency reconfiguration mechanism of a PIN diode on a reconfigurable antenna for LTE and WLAN Applications
Published 2018“…The antenna operates at 2.686GHz for Long-Term Evolution (LTE2500) and 5.164GHz for Wireless Local Area Network (WLAN) applications. …”
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56
Firearm recognition based on whole firing pin impression image via backpropagation neural network
Published 2011“…Firearms identification is a vital aim of firearm analysis. The firing pin impression image on a cartridge case from a fired bullet is one of the most significant clues in firearms identification. …”
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Book Chapter -
57
Firearm recognition based on whole firing pin impression image via backpropagation neural network
Published 2011“…Firearms identification is a vital aim of firearm analysis. The firing pin impression image on a cartridge case from a fired bullet is one of the most significant clues in firearms identification. …”
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Proceeding Paper -
58
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Induced rolling moment for NACA4412 plain and flapped wing
Published 2010“…Purpose – The paper aims to compute rolling moments on a follower aircraft wing due to vortices generated by a plain and flapped NACA4412 wing using experimental particle image velocimetery (PIV) data. …”
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Article -
60
Investigation of the vortical flow around a reverse delta wing
Published 2011“…A six component force balance was used to obtain the CL for a reverse delta wing and a delta wing for comparison purposes. A simulation of the streamlines, velocity vectors and surface pressure contours was carried out using CFD software to show the characteristics of the flow over a reverse delta wing.…”
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Proceeding Paper