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Ahmed, Sajeer and Mathur, NB and Manisankar, C (2011) Evaluation of aerodynamic performance of sidewall compression intake relevant to air breathing propulsion vehicles for intake flow entry at M = 3.5. Project Report. National Aerospace Laboratories, Bangalore.
Sudhakar, S and Mishra , Shashank and Ramesh, G and Madhavan, KT and Ahmed, Sajeer (2011) Experimental Studies on SM4308 Airfoil at Low Reynolds Numbers. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.
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.
Sathia Narayanan, A and Ahmed, Sajeer and Viji, M (2009) Empirical Evaluation of Wall Interference Effects on a Laminar Supercritical Airfoil at Transonic Speeds. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2009), December 10-12, Bangalore.
Arivoli, D and Dodamani, Ravi and Ramesh, G and Ahmed, Sajeer (2009) Preliminary wind tunnel studies on Micro-Air Vehicles. Project Report. National Aerospace Laboratories, Bangalore.
Ahmed, Sajeer and Sudhakar, S (2009) Experimental Study on Pitch up Problem Associated with Compound Delta Wings of Combat Aircraft Configurations. Project Report. National Aerospace Laboratories, Bangalore.
Ahmed, Sajeer and Sudhakar, (2007) Flows on delta wing. Project Report. National Aerospace Laboratories, Bangalore.
Merchant, Laxmikant and Ahmed, Sajeer (2003) Investigation of Methods for the Alleviation of Supersonic Flow-Instability of a Pitot Air-intake. Project Report. National Aerospace Laboratories, Bangalore.
Ahmed, Sajeer (1998) Experimental investigation on cone cylinder bodies of elliptical and circular cross sections at M = 2.0 AIAA Paper 98-2727. In: 16th AIAA Applied Aerodynamics Conference, June 15-18, 1998, Albuquerque, NM.
Ahmed, Sajeer and Selvarajan, S (1991) Investigation of flow field on a hammerhead nose configuration at transonic speeds AIAA-91-1711. In: 22nd Fluid Dynamics, Plasma Dynamics amp; Lasers Conference, 24-26 Jun 1991, Honolulu, Hawaii.
Ahmed, Sajeer (1987) Effectiveness of vortex plate on the aerodynamic characteristics of MiG-21M aircraft model. Project Report. National Aerospace Laboratories, Bangalore.
Ahmed, Sajeer (1987) Surface pressure measurements in the strap-on boosters interference region of 1/180 scale PSLV configuration at supersonic speeds. Project Report. National Aerospace Laboratories, Bangalore.
Ahmed, Sajeer and Selvarajan, S (1987) Steady pressure measurements in the strap on boosters interference region of 1/40 scale PSLV configuration. Project Report. National Aerospace Laboratories, Bangalore.
Ahmed, Sajeer and Selvarajan, S and Varambally, BS and Sivaramakrishnan, AE and Pandyan, S (1987) Steady pressure measurements in the strap-on booster interference Region of 1/20 scale aslv configuration. Project Report. National Aerospace Laboratories, Bangalore.
Ahmed, Sajeer and Selvarajan, S (1986) Unsteady Pressure Measurements on Scaled Configurations of ASLV. Project Report. NAL, Bangalore.
Swamy, MS and Ahmed, Sajeer and Sreenath, GS (1978) Model support system interference on zero-lift drag at transonic speeds. In: 10th Conference on Aerodynamic Testing, 19-21 Apr 1978, California, USA.
Shivakumar Swamy, M and Ahmed, Sajeer and Sreenath, GS (1978) Model support system interfrenceon zero-lift drag at trasonic speeds AIAA - 78-809. In: AIAA conference.
Swamy, Shivakumara M and Dutta, AC and Ahmed, Sajeer (1977) Experimental studies on a two-dimensional supersonic mixed compression air intake at mach numbers of 0.76, 1.06, and 1.18. Technical Report. National Aeronautical Laboratory, Bangalore, India.
