Items where Subject is "AERONAUTICS > Research and Support Facilities (Air)"

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Number of items at this level: 28.

C

CTFD , (1988) Augmentation of Flosolver MK 2. Project Report. NAL, Bangalore.

D

Desai, SS and Jain, RK (1970) A method of curvature matching for two dimensional flexible plate wind-tunnel nozzles. AIAA Journal, 8 (11). pp. 2105-2106.

Deshpande, MD and Balaji, S and Milton, S.George (1994) Laminar Flow Fields Three-Dimensional Cavity. Technical Report. National Aerospace Laboratories, Bangalore, India.

J

Jain, Anjana and Vijayan, Kalyani (2004) Forbidden reflections from the aramid PPTA-A novel correlation13; with stacking faults. Bulletin of Material Science, 27 (1). pp. 47-50.

K

Kidambi, R (2013) Inviscid Faraday waves in a brimful circular cylinder. Journal of Fluid Mechanics, 724 . pp. 671-694. ISSN 0022-1120

Krishnamurthy, SJ and Srilatha, KR (2009) DEVELOPMENT AND VALIDATION OF DESIGN METHODOLOGIES AND DESIGN TOOLS TO ENABLE WIND TURBINE ROTOR/BLADES TO BE OPTIMIZED FOR LOW AND MODERATE WIND REGIMES: PART-I BASELINE DESIGN AND ANALYSIS OF WIND TURBINE ROTOR. Project Report. National Aerospace Laboratories.

N

Naidu, VPS and Garlin, Delphina (2011) Assessment of Color and Infra-Red Images using No-Reference Image Quality Metrics. In: Proceedings of NCATC 2011 .

Naidu, VPS and Narayana , Rao. P. Missile and Target Engagement Scenario in Matlab Simulink. MSDF Lab. (Unpublished)

Nilakantan, P (1963) High-speed wind tunnels for aerospace research. Technical Report. National Aeronautical Laboratory, Bangalore, India.

P

Parameswaran, V and Mary Preena, M (1998) Recursive Estimation of Model Error for Identifi- cation of Non-Linear Continuous Time Systems. Technical Report. National Aerospace Laboratories, Bangalore, India.

Parida, BK and Prakash, Raghu V (1993) First Omarterly Review Meeting - A Project SN-0-101. Technical Report. National Aerospace Laboratories, Bangalore, India.

Poornima, N and Senthil Kumaran, R and Jagannatha Rao, B and Swamy, KMM (2009) Instrumentation and Data Acquisition System For Large Scale Rotating Rig. Technical Report. National Aerospace Laboratories.

R

Rajamurthy, MS and Basappa, - (1995) Generation of Comprehensive Aerodynamic Data Using Dynamic Wind Tunnel Simulation. Technical Report. National Aerospace Laboratories, Bangalore, India.

Raju, Channa and Viswanath, PR (2005) Pressure-Sensitive Paint Measurements in a Blowdown Wind Tunnel. Journal of Aircraft, 42 (4). pp. 908-915. ISSN 0021-8669

Ram, Mohan VS and Srinath Sastry, CV (1986) Non-linear maximum likelihood estimation of stability derivatives from range data. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Ramaswamy, Setty J and Dayananda, GN and Subba Rao, M (2007) Development of a Door Steering Mechanism for a Large Autoclave. In: National Conference on Recent Advances in Design Engineering, 22-24 Feb 2007, Manipal.

Ravishankar, S and Dutt, HNV and Gurumoorthy, B (2010) Automated inspection of aircraft parts using a modified ICP algorithm , H. N. V. Dutt and B. International Journal of Manufacturing Technology, 46 (1-4). pp. 227-236.

S

Senthil Kumar, P and Jayasankar, S and Satisha, Vishwanath and Sateesh, VL and Kamaleshiah, MS and Dayananda, GN (2013) Development and wind tunnel evaluation of an SMA based trim tab actuator for a civil aircraft. SMART MATERIALS AND STRUCTURES, 22 (9).

Senthil Kumaran, R and Swamy, KMM (2007) CASCADE TESTS ON CE 20 LOX TURBINE NOZZLE BLADE PROFILE. Technical Report. National Aerospace Laboratories.

Senthil Kumaran, R and Swamy, KMM (2006) CASCADE TESTS ON CE 20 LOX TURBINE SECOND ROTOR BLADE PROFILE. Technical Report. National Aerospace Laboratories, Bangalore.

Shantha Kumar, N (1995) Sensor Failure Detection and Management Scheme for Pressure Probes Kalman Filtering Technique. Technical Report. National Aerospace Laboratories, Bangalore, India.

Sharath, PP and Senthil Kumaran, R and Jagannatha Rao, B and Poornima, N (2009) CALIBRATION OF PITOT STATIC PROBES FOR HAL, KORAPUT. Technical Report. National Aerospace Laboratories, Bangalore.

Subramanian, NR (1965) Application of rheoelectrical analogy to the study of wind tunnel contraction (Wind tunnel contraction study of inviscid incompressible flow using rheoelectrical analogy, discussing experimental techniques, contour velocity distribution, optimum smoke injector and adverse pressure gradient estimation). Aeronautical Society of India, Journal, 17 . pp. 154-166.

Sudesh, K and Shantha Kumar, N and Girija, G and Raol, JR (2003) Sensor data characterisation and fusion and fusion for target tracking applications. In: International Radar Symposium, 2003, India.

Sundaramurthy, H (1981) A sensitive rolling moment balance for use in supersonic blowdown tunnels AIAA-81-4237. Journal of Aircraft, 18 (9). pp. 799-800. ISSN 0021-8669

Swamy, KMM and Senthil Kumaran, R (2009) ESTIMATION OF TURBOMACHINERY FLOW LOSSES THROUGH CASCADE TESTING. In: LOSS MECHANISMS IN STEAM AND GAS TURBINES, 17-07-2009 to 18-07-2009, M.S.Ramiah School of Advanced Studies, Bangalore, India.

V

Venkatakrishnan, L (2004) Comparative Study of Different Pressure-Sensitive-Paint13; Image Registration Techniques. AIAA Journal, 42 (11). pp. 2311-2319. ISSN 0001-1452

Venkatakrishnan, L and Meier, G E A (2004) Density measurements using the Background Oriented13; Schlieren technique. Experiments in Fluids, 37 (2). pp. 237-247. ISSN 0723-4864

This list was generated on Mon Dec 22 01:04:27 2014 IST.