Published: May 31, 2016

Effect of Flexibility and Aircraft Flow Field on Rail Launch Simulation of a Missile

Shaik Ismail (1), P. C. Jain (2), P. S. R. Anjaneyulu (3)
(1) Scientist Defence Research and Development Laboratory (DRDL) Kanchanbagh Post,Hyderabad-500 058 ,
(2) Scientist Defence Research and Development Laboratory (DRDL) Kanchanbagh Post,Hyderabad-500 058 ,
(3) Scientist Defence Research and Development Laboratory (DRDL) Kanchanbagh Post,Hyderabad-500 058
81-88
147

Effect of Inlet Vane Angle of a Partial Vane Diffuser on the Performance and Flow Filed of a Centrifugal Compressor

S. Anish (1), N. Sitaram (2)
(1) Department of Mechanical Engineering National Institute of Technology Suratkal Suratkal-575 025, Karnataka ,
(2) Thermal Turbomachine Laboratory Department of Mechanical Engineering Indian Institute of Technology Madras Chennai-600 036
89-100
40

Design Point Parameter Estimation of a Legacy Twin Spool Turbojet Engine for Health Monitoring

Balaji Sankar (1), Brijeshkumar Shah (2), Soumendu Jana (3), Ramamurthy Srinivasan (4), R. K. Satpathy (5), G. Gouda (6)
(1) CSIR National Aerospace Laboratories (NAL) HAL Airport Road, Post Box No. 1779 Bangalore-560 017 ,
(2) CSIR National Aerospace Laboratories (NAL) HAL Airport Road, Post Box No. 1779 Bangalore-560 017 ,
(3) CSIR National Aerospace Laboratories (NAL) HAL Airport Road, Post Box No. 1779 Bangalore-560 017 ,
(4) CSIR National Aerospace Laboratories (NAL) HAL Airport Road, Post Box No. 1779 Bangalore-560 017 ,
(5) Regional Center for Military Airworthiness (RCMA) HAL Koraput Engine Division Orissa ,
(6) Regional Center for Military Airworthiness (RCMA) HAL Koraput Engine Division Orissa
101-109
43

A Note on Single Impulse Approach for Trajectory Correction

R.B. Sarsar (1), S.D. Naik (2), P.V. Arlulkar (3)
(1) Armament R & D Establishment (ARDE) Pashan, Pune-411 021 ,
(2) Armament R & D Establishment (ARDE) Pashan, Pune-411 021 ,
(3) Defence Institute of Advanced Technology (DIAT) Girinagar, Pune-411 025
110-116
35

Human Factors, Analysis Tools and Methods for Development of Reliable Aircraft Design

Archana Hebbar (1), Abhay A Pashilkar (2)
(1) Scientist CSIR-National Aerospace Laboratories (NAL) Kodihalli Post, HAL Airport Road Bangalore-560 017 ,
(2) Senior Principal Scientist CSIR-National Aerospace Laboratories (NAL) Kodihalli Post, HAL Airport Road Bangalore-560 017
117-127
28

Thermal and Mechanical Analysis of FGM Beam Using Generalized Theory

Dinesh Kumar (1), Kanishk Sharma (2)
(1) Assistant Professor Department of Mechanical Engineering Malaviya National Institute of Technology Jaipur Jaipur-302 017 ,
(2) Ph.D Research Scholar Department of Mechanical Engineering Malaviya National Institute of Technology Jaipur Jaipur-302 017
128-140
29

Airborne Separation Assistance during Landing - An Approach for Automation

B. Padmashree (1), B. Subba Reddy (2)
(1) VTU Extension Centre - Honeywell Honeywell Technology Solutions Lab Pvt Ltd No. 151/1, Doraisanipalya, Bannerghatta Road Bangalore-560 076 ,
(2) VTU Extension Centre - Honeywell Honeywell Technology Solutions Lab Pvt Ltd No. 151/1, Doraisanipalya, Bannerghatta Road Bangalore-560 076
141-146
134