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Number of items: 11.

Krishnan, V and Mathur, NB (1997) Afterbody Boundary Layer Measurements in the Base Flow Facility. Technical Report. National Aerospace Laboratories, Bangalore,India.

Krishnan, V and Viswanath, PR and Rudrakumar, S (1997) Effect of riblets on axisymmetric base pressure. Journal of Spacecraft and Rockets, 34 (2). pp. 256-258. ISSN 0022-4650

Kumar, Rajeev and Viswanath, PR (1997) The Influence of a Forward Splitter Plate on Base Pressure and Drag of Wedges. Technical Report. National Aerospace Laboratories, Bangalore, India.

Rajeev Kumar, - and Viswanath, PR (1997) The Influence of a Forward Splitter Plate on Base Pressure and Drag of Wedges. Technical Report. National Aerospace Laboratories, Bangalore,India.

Raju, Channa and Viswanath, PR (1997) Base drag reduction due to riblets on a gaw (2) airfoil. Technical Report. National Aerospace Laboratories, Bangalore, India.

Ramesh, G (1997) Development of an Interrogation System for Particle Imaging Velocimetry. Technical Report. National Aerospace Laboratories, Bangalore,India.

Sajeer, Ahmed and Venkatasuramanyam, DV and Rao, RMVGK (1997) Preparation Of 1 :4.405 And 1 :7.645 Scale LCA Air Intake Models For Tests at ONERA. Technical Report. NAL, Bangalore.

Sundaram, S and Grosche, FR and Kreplin, HP (1997) Cross-correlation measurements in Naturally Occurring Tollmien-Schlichting Waves. Technical Report. National Aeronautics and Space Administration.

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

Yegna Narayan, K and Seshadri, SN (1997) Types of flow on the lee side of delta wings. Progress in Aerospace Sciences, 33 (3-4). pp. 167-257. ISSN 0376-0421

Yegna Narayan, K and Seshadri, SN (1997) Types of flow on the lee side of delta wings13. Progress in Aerospace Sciences, 33 (3-4). pp. 167-257.

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