Browse by Department
Number of items: 12.
Conference or Workshop Item
Kumar , R and Venkatakrishnan, L and Wiley, Alex and Alvi, Farukh (2010) Role of coherent structures in supersonic impinging jet noise and its control. In: 16th AIAA/CEAS Aeroacoustics Conference, 7-9 Jun 2010, Stockholm, Sweden.
Manisankar, C and Sajeer, Ahmed and Thiagarajan, V (2010) Investigation of starting process of a movable intake configuration at high supersonic speeds. In: Proceedings of the 13th Asian Congress of Fluid Mechanics, 17-21 Dec 2010, Dhaka, Bangladesh.
Karthikeyan, N and Venkatakrishnan, L (2010) Application of photogrammetry to surface flow visualization. Experiments in Fluids, 49 (9). pp. 1-10. ISSN 0723-4864
Mandal, AC and Venkatakrishnan, L and Dey, J (2010) A study on boundary-layer transition induced by free-stream turbulence. Journal of Fluid Mechanics, 660 . pp. 114-146. ISSN 0022-1120
Verma, SB and Haidn, O (2010) Flow characteristics of overexpanded rocket nozzles. International Journal of Aerospace Innovations, 2 (4). pp. 259-277. ISSN 1757-2258
Verma, SB and Stark, R and Nuerenberger-Genin, C and Hakin, O (2010) Cold-gas experiments to study the flow separation characteristics of a dual-bell nozzle during its transition modes. Shock Waves, 20 . pp. 191-203.
Hemant , Sharma (2010) Feasibility Study Conducted for the Development of an Autonomous mini Unmanned Air Vehicle. Project Report. National Aerospace Laboratories, Bangalore.
Mathur, NB and Viji, M (2010) Experimental studies on twinjet afterbody-nozzle system of combat aircraft configurations. Project Report. National Aerospace Laboratories, Bangalore.
Mukund, R and Chandan Kumar, A (2010) Experiments on NAL 21463 airfoil in the 1.5m wind tunnel for NAL RTA. Project Report. National Aerospace Laboratories, Bangalore.
Ramesh, G and Madhavan, KT and Ahmed, Sajeer and Sudhakar, (2010) Development of synthetic Jet based flow control technique for Low Revnolds number applications. Project Report. NAL, Bangalore.
Sajeer, Ahmed and Sudhakar, S (2010) Experimental Study on Pitch up Problem Associated with Compound Delta Wings of Combat Aircraft Configurations. Project Report. National Aerospace Laboratories, Bangalore.
Verma, SB and Channa Raju, - and Manisankar, C (2010) Shock-wave boundary-layer interaction study on a 20 deg compression corner using PSP and Kulites. Project Report. National Aerospace Laboratories, Bangalore.