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Institution

National Aerospace Laboratories

FacilityBengaluru, India
About: National Aerospace Laboratories is a facility organization based out in Bengaluru, India. It is known for research contribution in the topics: Coating & Corrosion. The organization has 1838 authors who have published 2349 publications receiving 36888 citations.


Papers
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Journal ArticleDOI
TL;DR: In this article, phase analysis, morphology and electronic structure of the as-grown and annealed thin films are respectively investigated by X-ray diffraction (XRD), field emission scanning electron microscopy (FESEM) and Xray photoelectron spectroscopy (XPS) techniques.

11 citations

Journal ArticleDOI
TL;DR: In this paper, an optimized tandem absorber with reactive gas flow rate was studied using the thickness data, target voltage and target current, which indicated a decrease in the growth rate of each individual layer with an increase in the flow rates of the reactive gases.

11 citations

Journal ArticleDOI
TL;DR: In this article, a method for estimating the power spectrum of a complex signal (CS) realised by the group delay (GD) for a CS and the modified GD concept is proposed.
Abstract: A method for estimating the power spectrum of a complex signal (CS) realised by the group delay (GD) for a CS and the modified GD concept is proposed This extends the performance advantages of the modified GD applicable to a real signal to a complex signal A significant reduction in variance without any compromise in frequency resolution over that of the periodogram is found

11 citations

Journal ArticleDOI
TL;DR: In this article, the effect of freestream flow and cowl-length variation on upstream flow interference effects and the base wake-closure nozzle pressure ratio was investigated and it was shown that increasing the cowl length significantly reduces the upstream interference effects.
Abstract: An experimental investigation has been carried out to study the effect of freestream flow and cowl-length variation on (i) upstream flow interference effects and (ii) the base wake-closure nozzle pressure ratio. It is observed that for supersonic freestream Mach numbers the nozzle exhaust seems to only slightly influence the upstream interference effects for M = 1.2 but shows significant influence for M = 1.6. Increasing the cowl-length further reduces the upstream flow interference effects significantly. Further, the reduced momentum thrust from the inner nozzle in the presence of freestream for similar nozzle pressure ratio (relative to static tests) delays the downstream movement of the system of shocks on the plug surface. In the case of the plug truncated at 40% length, this delays the onset of base-wake closure and hence, increases the base-wake closure nozzle pressure ratio with increasing freestream Mach number. Increasing the cowl-length also helps to increase the base pressure thrust contribution at all operating conditions.

11 citations

Proceedings ArticleDOI
21 Jul 2016
TL;DR: This paper explores the evolution of a reliable, robust Vad scheme for VOS application in aircraft by comparing real-time robust VAD schemes, which are based on energy-based detectors, fuzzy logic and ANN.
Abstract: In a fighter aircraft, for the optimal usage of resources during transmission of signals, a Voice Operated Switch (VOS) is used, as it is considered as a better option compared to push to talk (PTT), because it gives hands free environment for the pilot to carry out other crucial tasks. The heart of VOS is a Voice Activity Detection (VAD) algorithm. This paper explores the evolution of a reliable, robust VAD scheme for VOS application in aircraft by comparing real-time robust VAD schemes, which are based on energy-based detectors, fuzzy logic and ANN. MATLAB, is used as the simulation platform and actual fighter aircraft cockpit noise record is used for evaluation of the algorithms.

11 citations


Authors

Showing all 1850 results

NameH-indexPapersCitations
Harish C. Barshilia462366825
K.S. Rajam42834765
Kozo Fujii394115845
Parthasarathi Bera391365329
R.P.S. Chakradhar361664423
T. N. Guru Row363095186
Takashi Ishikawa361545019
Henk A. P. Blom341685992
S. Ranganathan332115660
S.T. Aruna331014954
Arun M. Umarji332073582
Vinod K. Gaur33924003
Keisuke Asai313503914
K. J. Vinoy302403423
Gangan Prathap302413466
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Performance
Metrics
No. of papers from the Institution in previous years
YearPapers
202310
202216
2021143
2020100
201996
2018119