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Number of items: 24.

B

Bera, Rajendra K (1976) Aircraft external stores wind tunnel techniques and scaling laws. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Bera, Rajendra K (1976) On simulation and evaluation of aircraft handling qualities. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Bera, Rajendra K and Ramachandra, SM (1976) Some theorems concerning drag minimization. Revue Roumaine des Sciences Techniques, Serie de Mecanique Appliquee, 21 . pp. 523-529.

D

Desikan, KS (1976) Design of prototype intake silencer for 60mw fd fan (BHEL). Technical Report. National Aeronautical Laboratory, Bangalore, India.

K

Kanagarajan, V (1976) Experimental studies on a wing with strake. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Kumar, Anand and Yajnik, K (1976) Poiseuille flow development by eigenfunction expansion method. Technical Report. National Aeronautical Laboratory, Bangalore, India.

L

Leelavathi, K and Rajappa, N (1976) Operational validation of a computer program to calculate incompressible potential flow past a lifting airfoil by the method of catherall foster and sells. Technical Report. National Aeronautical Laboratory, Bangalore, India.

M

Mahalingam, V and Srikantan, KV and Mahalingam, R and Nagabhushana, S and Krishnamurthy, DR and Raghumurthy, G (1976) Redesign of the memory in digital data acquisition system of the NAL 4-Ft. trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

N

Narayan, G and Mahalingam, V and Srikantan, KV and Mahalingam, R (1976) Receiver oscillation studies. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Narayana, CL and Sinha, AK and Ramamoorthy, P (1976) Estimation of drag-divergence mach number for an airfoil. Technical Report. National Aeronautical Laboratory, Bangalore, India.

P

Prabhu, KR (1976) Drag prediction methods for prelimanary design of an aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Prabhu, KR (1976) Drag prediction methods for preliminary design of an aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.

R

Ramamoorthy, P and Padmavathi, K (1976) Airfoil design by optimisation. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Ramamoorthy, P and Sinha, AK and Narayana, CL and Dutta, Vimala and Dwarakanath, GS and Sheela, BV (1976) Optimization of a passenger aircraft for minimum direct operating cost - A preliminary study. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Rangarajan, R and Ramaswamy, MR (1976) Design of 2nd DIA strain gauge balance with replaceable axial force unit. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Rao, DM and Murthy, AV and Kashyap, RR (1976) A variable by-pass diffuser for supersonic wind tunnels. Journal of Aeronautical Society of India, 28 . pp. 27-31.

Rao, DM and Seshadri, SN (1976) Application of Radial-Splitters for Improved wide-angle diffuser performance in blowdown tunnel. Journal of Aircraft, 13 (7). pp. 538-540. ISSN 0021-8669

S

Sarasamma, VR (1976) Smoothening of airfoil coordinates. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Shankar, PN (1976) Effects of geometry and reynolds number on savonious type rotors. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Shankar, PN and Sinha, UN (1976) The Rayleigh problem for a wavy wall (impulsive motion generation of viscous fluid flow). Journal of Fluid Mechanics, 77 . pp. 243-256. ISSN 0022-1120

Sundar murthy, H and Prasada Rao, K (1976) A half model free oscillation fot pitch damping measurements. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Sundaramurthy, H and Narayana, T (1976) A free-oscillation test rig for pitch-damping measurements in N.A.L. trisonic wind tunnels. Journal of Aeronautical Society of India, 28 . pp. 227-230.

Y

Yajnik, KS and Gupta, Ramesh P (1976) Strong interaction effects on upstream wall pressure in a separated flow with a forward-facing wall jet. In: AIAA 1976, 4-16 July 1976, United States.

Yajnik, KS and Subbaiah, MV (1976) Representation of the drag polar of a fighter aircraft. Journal of Aircraft, Vol. 1 . pp. 155-156. ISSN 0021-8669

This list was generated on Mon Apr 21 01:16:16 2014 IST.