Items where Author is "Rao, DM"

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Number of items: 13.

Journal Article

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

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 (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.

Rao, DM (1971) A method of flow stabilisation with high pressure recovery in short, conical diffusers. The Aeronautical Journal, 75 . pp. 336-339.

Rao, DM (1970) Hypersonic aerodynamic characteristics of flat delta and caret wing models at high incidence angles. Journal of Spacecraft and Rockets, 7 (12). pp. 1475-1476.

Proj.Doc/Technical Report

Murthy, AV and Rao, DM (1975) Pilot ludwieg tube project. 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.

Dwarakanath, GS and Ramamoorthy, P and Rao, DM (1974) Evaluation of the transonic wave drag integral with particular reference to a real aircraft. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Seshadri, SN and Rao, DM (1974) On the application of radial-splitters flow spreaders in the NAL 1-FT. blowdown tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Rao, DM and Raju, KN (1964) The use of splitters for flow control in wide angle conical diffusers. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Rao, DM (1961) Some aspects of design of air storage system for blowdown wind tunnels. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Rao, DM and Nilakantan, P (1960) Note on compressed air capacity requirements for the 4-FT. Trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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