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Number of items: 22.

Journal Article

Bera, Rajendra K (1975) On the wave drag integral for slender bodies. Journal of Aircraft, 12 (11). pp. 908-910. ISSN 0021-8669

Matsuzaki, R (1975) Nonequilibrium flow of nitrogen behind a strong normal shock wave. Physical Society of Japan, 39 . pp. 1608-1613.

Murthy, AV (1975) Hypersonic flow over concave surfaces with leading-edge bluntness. AIAA Journal, 13 (9). pp. 1230-1233. ISSN 0001-1452

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

Rao, DM (1975) Hypersonic incipient separation on delta wing with trailing-edge flap. AIAA Journal, 13 (10). pp. 1386-1388. ISSN 0001-1452

Rao, DM (1975) Separated flow induced by trailing-edge flaps on delta wings at M = 8.2. Journal of Aeronautical Society of India, 27 . pp. 17-21.

Sheela, BV and Ramamoorthy, P (1975) SWIFT - A new constrained optimization technique (Sequential Weight Increasing Factor Technique for nonlinear programming). Computer Methods in Applied Mechanics and Engineering, 6 (3). pp. 309-317. ISSN 0045-7825

Vimala, CS and Nath, G (1975) Mass transfer effectiveness on three-dimensional laminar compressible boundary layer flows. Journal of Fluids Engineering, 97 . pp. 382-384.

Proj.Doc/Technical Report

Bera, Rajendra K (1975) Functional approximations to experimental data. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Bera, Rajendra K (1975) Functional approxmations to experimental data. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Mahalingam, V and Srikantan, KV and Balakrishna, S (1975) Modification of the model incidence control system of the NAL 4-ft. trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Murthy, AV and Rao, DM (1975) Pilot ludwieg tube project. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Narayan, G and Mahalingam, V and Srikantan, KV (1975) Pressure sweep generator for the NAL 4-ft trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Narayan, G and Mahalingam, V and Srikanthan, KV (1975) Presure sweep generator for the NAL 4-ft trisonic wind tunnel. Technical Report. National Aerospace Laboratories, Bangalore,India.

Parameswaraiah, R and Murthy, Sreedhara (1975) Electronic microwelding power generator for fabricating hot wire probes used in fluid flow studies. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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

Rao, DM and Rajendra, G and Sundaramurthy, H and Kanagarajan, V (1975) Contributions by NAL Aerodynamics Division at SLV-3 Review. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Shankar, PN (1975) On the aerodynamics performance of a class vertical axis windmills. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Srikantan, KV (1975) Transonic mach number sweep system for the NAL 4'x4' trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Srikantan, KV and Mahalingam, V (1975) Blowdown sequence-sequential logic display for the N.A.L.4'*4' trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Yajnik, KS (1975) Energy turn rate characterstic of an aircraft and turn performance. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Yajnik, KS and Subbaiah, MV (1975) On the representation of the drag polar of a fighter aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.

This list was generated on Thu Sep 18 01:16:15 2014 IST.