Items where Author is "Ramaswamy, MA"

Up a level
Export as [feed] RSS 2.0 [feed] RSS 1.0 [feed] Atom
Group by: Item Type | No Grouping
Number of items: 25.

Ramaswamy, MA and Narasimhaswamy, KN (1991) Flow Visualisation Studies On Wall Mounted Pitot Type Intake With Splitter Plate. Technical Report. NAL, Bangalore.

Patil, SR and Ramaswamy, MA (1988) Development of experimental techniques for helicopter rotor performance studies. Aeronautical Society of India, Vol. 4 (3). pp. 201-209.

Singh, JP and Rangarajan, R and Ramaswamy, MA (1988) Computation of flow over airfoils under high lift separated flow condition 13; 13;. Journal of Aeronautical Society of India, 40 . pp. 105-110.

Patil, SR and Ramaswamy, MA (1988) Development of Experimental Techniques to determine the Aerodynamic Performance of Helicopter Rotors in Hover and Forward Flight - Closure Report for AR & DB Project AE-0-154. Project Report. National Aerospace Laboratories, Bangalore.

Nandanan, M and Ramaswamy, MA (1987) Lifting symmetric supercritical airfoils for wing design of combat aircraft 13; 13;. Communications in Applied Numerical Methods, Vol. 3 . pp. 463-468. ISSN 0748-8025

Patil, SR and Ramaswamy, MA (1987) Model helicopter rotor rig and associated strain gauge balance for performance studies. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Patil, SR and Ramaswamy, MA (1987) Development of Experimental Techniques to Determine the Aerodynamic Performance of Helicopter Rotors in Hover and Forward Flight - Progress Report for 1986-87. Project Report. National Aerospace Laboratories, Bangalore.

Nandanan, M and Ramaswamy, MA (1986) Aerodynamic characteristics of lifting symmetric supercritical airfoils. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Patil, SR and Raman, KS and Ramaswamy, MA (1986) Development of Experimental Techniques to Determine the Aerodynamic Performance of Helicopter Rotors in Hover and Forward -Flight - Progress Report for 1985-86. Project Report. NAL, Bangalore.

Patil, SR and Raman, KS and Ramaswamy, MA (1986) Analysis of a special short wind tunnel internal strain gauge balance and comparison with experimental calibration data. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Singh, JP and Rangarajan, R and Ramaswamy, MA (1985) Computatian of flow over airfoils under high 11ft separated flow conditions. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Singh, JP and Rangarajan, R and Ramaswamy, MA (1985) Computatian of flow over airfoils under high 1ift separated flow conditions. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Nandanan, M and Ramaswamy, MA (1985) Design of lifting symmetric supercritical airfoils. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Nandanan, M and Ramaswamy, MA (1985) Supercritical wing design for combat aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Ramaswamy, MA and Desikan, KS (1978) Annular sleeve type control valve with radial outflow for blowdown wind tunnels. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Ramaswamy, MA and Rajendra, G (1978) Experimental investigation of transonic flow past a blunt cone-cylinder. Journal of Spacecraft and Rockets, 15 (2). pp. 120-123. ISSN 0022-4650

Desai, SS and Viswanathan, S and Ramaswamy, MA (1977) Numerical evaluation of transonic wave drag. Journal of Aircraft, 14 (2). pp. 215-217. ISSN 0021-8669

Ramaswamy, MA and Viswanathan, S (1975) Some observations on the Adams body of minimum wave drag. Journal of Aircraft, 12 . pp. 1001-1002. ISSN 0021-8669

Ramaswamy, MA and Parikh, PC (1975) Pressure distribution of aerofoils if embedded supersonic region. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Ramaswamy, MA and Sharma, Ramachandra and Krishnamuthy, K (1974) Two dimentional transonic blockage interference studies in the NAL 1-Ft. blowdown wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Ramaswamy, MA (1974) Application of integral moment method to the hypersonic laminar near wake of a cold cylinder. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Sinha, UN and Ramaswamy, MA (1974) Preliminary results of the computation of pressure distribution on a super critical aerofoil. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Sinha, UN and Ramaswamy, MA (1974) Priliminary results of the computation of pressure distribution on a supercritical aerofoil. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Ramaswamy, MA and Kubota, Toshi (1972) Near wake of a cold circular cylinder AT M=6. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Ramaswamy, MA (1961) Design of transonic test-sections for blowdown wind tunnels. Technical Report. National Aeronautical Laboratory, Bangalore, India.

This list was generated on Thu Nov 27 02:53:00 2014 IST.