Items where Author is "Patil, SR"

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Number of items: 19.

Viswanath, PR and Patil, SR (1997) Zero-lift drag characteristics of afterbodies with a square base. Journal of Spacecraft and Rockets, 34 (3). pp. 290-293. ISSN 0022-4650

Vishwanath, PR and Patil, SR and Verma, RS (1996) Direct Drag Measurements On Two LCA- Related Afterbodies Using The Jet Simulation Rig. Technical Report. NAL, Bangalore.

Vishwanath, PR and Patil, SR and Verma, RS (1996) Direct Drag Measurements On Two LCA-Related Afterbodies Using The Jet Simulation Rig. Technical Report. NAL, Bangalore.

Patil, SR (1994) Buffet tests on 1/20 scale lca model with leading edge slats at transonic speeds. Project Report. National Aerospace Laboratories, Bangalore.

Viswanath, PR and Patil, SR (1994) Aerodynamic characteristics of delta wing-body combinations at high angles of attack. Aeronautical Journal, 98 (975). pp. 159-170.

Viswanath, PR and Patil, SR (1994) Aerodynamic characteristics of delta wing-body combinations at high angles of attack. Aeronautical Journal, 98 (975). pp. 159-170. ISSN 0001-9240

Patil, SR and Pandian, S (1991) Force Measurements On 1/20th Scale ASLV Model With Relocation of SITVC Tanks. Technical Report. NAL, Bangalore.

Patil, SR and Pandyan, S (1991) Force Measurements On 1/24th Scale Model Of ASLV With Eight Sitvic Tanks. And All Protrusions (Aslv-D3 Configuration). Technical Report. NAL , Bangalore .

Klaus, Hartmann and Patil, SR (1991) Experimental investigations on wing-body combinations and their components at high angles of attack in the subsonic and transonic speed range (Rumpf, gestutzter deltafluegel, stroemungsabloesung, kraft-und momenttenmessung, interferenzen). Technical Report. National Aeronautical Laboratory, Bangalore, India.

Viswanath, PR and Patil, SR (1990) Effectiveness of passive devices for axisymmetric base drag13; reduction at mach 2. Journal of Spacecraft and Rockets, 27 (3). pp. 234-237.

Patil, SR and Sridharan, R (1989) Wind tunnel wall corrections to experimental data on wing-body combinations at high angles of attack. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Viswanath, PR and Patil, SR (1988) Performance of passive devices for axisymmetric base drag reduction at mach 2. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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.

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.

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.

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 (1986) A brief documentation on small helicopter rotor models with13; rigid blades. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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.

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