Items where Author is "Sundaramurthy, H"

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Sundaramurthy, H (2009) Statistical analysis of repeat test results for assessment of wind tunnel data quality. In: National Conference on Wind Tunnel Testing (2009-IT2), 12-14 Mar 2009, IISc., Bangalore.

Gireesh , Yanamashetti and Jagadeeswarachar, SP and Sundaramurthy, H (2007) A Description Of Sub-Systems And Calibration Formulations Of The NAL Automatic Balance Calibration System (ABCS). Technical Report. NAL, Bangalore.

Sundaramurthy, H (2005) Method for static divergence analysis of sting-mounted wind tunnel models. Technical Report. National Aerospace laboratories, Bangalore, India.

Sundaramurthy, H and Verma, RS and Jagadeeswarachar, SP and Kumar, Rajan (2001) Flow quality improvements in a blowdown wind tunnel 13; 13;. Journal of Aircraft, 38 (3). pp. 577-580.

Sridhar, PS and Manimekalai, B and Sundaramurthy, H (1999) Data Acquisition and Processing for Measurements of Start/Stop Loads from the NAL-0.6m Blowdown Wind Tunnel. In: 118th Supersonic Tunnel Association International (STAI), 11Oct 2012, BRUSSELS, BELGIUM.

Rajan Kumar, - and Sundaramurthy, H and Prasada Rao, K (1997) Unsteady Pressure Measurements On 1 :40 Scale GSLV Heat Shield Model. Project Report. National Aerospace Laboratories, Bangalore.

Sundaramurthy, H and Suryanarayana, GK and Lochan, R and Sivaramakrishnan, AE and Pandian, S (1995) Wind tunnel simulation of multibooster separation trajectories of a launch vehicle. Journal of Spacecraft and Rockets, 32 (3). pp. 561-563.

Sundaramurthy, H (1993) An overview of some aspects of Combat Aircraft Spin. Technical Report. National Aerospace Laboratories, Bangalore, India.

Verma, RS and Sundaramurthy, H (1990) Design Features And Stress Analysis Of A 0.686-Scale Standard Dynamics Model. Technical Report. NAL, Bangalore.

Nagarajan, V and Sundaramurthy, H (1990) Measurement Of Pitch-Damping Derivatives On Prithvi Model In The Nal 1.2m Tunnel. Technical Report. NAL, Bangalore.

Sundaramurthy, H and Suryanarayana, GK (1987) Wind tunnel simulation of PSLV strap-on booster separation trajectories. Project Report. National Aerospace Laboratories, Bangalore.

Sundaramurthy, H and Narayan, KY and Suryanarayana, GK and Lochan, Rajeev and Sasidharan Nair, KG (1986) Wind tunnel investigation of strap-on booster separation characteristics of a launch vehicle. In: 2nd National Conference on Aerodynamics, 19-20 Dec 1986, Bangalore, India.

Ramabhadran, S and Sundaramurthy, H (1986) A Computer programme for DATCOM methods of estimation of lateral stability and control derivatives. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Sundaramurthy, H and Narayan, KY and Suryanaraya, GK and Lochan, Rajeev and Sasidharan Nair, KG (1986) Wind tunnel investigation of strap-on booster separation13; characteristics of a launch vehicle. Journal of Aeronautical Society of India, 38 . pp. 215-221.

Bhagawan, BS and Parameswaran, V and Rajeswari, Ramamurthy and Sridhar, JK and Srinatha Sastry, CV and Ramabhadran, S and Seshadri, SN and Sundaramurthy, H and Yegnanarayan, K (1985) Stability and Control characteristics of MIG-21 aircraft. Project Report. National Aerospace Laboratories, Bangalore.

Sundaramurthy, H (1983) Review of scaling requirements for wind tunnel model for dynamic investigations. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Sundaramurthy, H (1983) Review of scaling requirements for wind tunnel models for dynamic investigations. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Nagarajan, V and Sundaramurthy, H (1982) Estimation of inertial peoperties of wind tunnel aircraft models Part I: Development of a computer programme13; Part II: Description of a rig and measurements on typical models. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Sundaramurthy, H (1981) A sensitive rolling moment balance for use in supersonic blowdown tunnels AIAA-81-4237. Journal of Aircraft, 18 (9). pp. 799-800. ISSN 0021-8669

Sundaramurthy, H and Jategaonkar, RV and Rao, Prasada K and Vasudeva, NS (1978) A forced-oscillation rig for dynamic stability measurements in NAL high speed wind tunnels. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Sundaramurthy, H and Jategoankar, RV and Balakrishna, S (1978) Dynamic stability measurements from tunnel unsteadiness excited random response AIAA-78-831. In: 10th Aerodynamic Testing Conference.

Sundaramurthy, H (1978) Validity of axis transfer technique for pitch damping measurements AIAA-78-833. In: 10th Aerodynamic Testing Conference.

Sundaramurthy, H and Narayana, T (1976) A free-oscillation test rig for pitch-damping measurements in N.A.L. trisonic wind tunnels. Journal of Aeronautical Society of India, 28 . pp. 227-230.

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.

Sundaramurthy, H and Narayana, T and Gurjale, AK (1973) Free oscillation testing on a sting-mounted 25 cone model in the NAL 4-foot trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Sundaramurthy, H (1972) Dynamic stability testing in wind tunnels. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Sundaramurthy, H and Gurjale, AK and Gopala, KV (1971) Description and calibration of the 2quot;x10quot; induction tunnel (with and without plenum chamber suction). Technical Report. National Aeronautical Laboratory, Bangalore, India.

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