Browse by Department
Number of items: 22.
AAnand, kumar (1988) Euler solutions with a multi-block structured code 13; 13;. Journal of Aeronautical Society of India, 40 . pp. 89-95. BBera, Rajendra K (1988) Quadrature formula for a double-pole singular integral ((in linear lifting surface theory). AIAA Journal, 26 . pp. 752-754. ISSN 0001-1452 CChakrabartty, SK and Subramanian, NR (1988) Computation of 3-D transonic flows for wings and wing-body configurations. Technical Report. National Aeronautical Laboratory, Bangalore, India. DDeshpande, MD and Shankar, PN (1988) Experiments on liquid vapour phase change between plane liquid surfaces part:3 results from a closed quartz chamber. Technical Report. National Aeronautical Laboratory, Bangalore,India. Dutta, Vimala (1988) LAWS-Lift analysis of wings in supersonic flows. Technical Report. National Aeronautical Laboratory, Bangalore, India. Dutta, Vimala (1988) Solution of one-dimensional euler-equations by the implicit finite difference technique of beam and warming. Technical Report. National Aeronautical Laboratory, Bangalore, India. Dutta, Vimala and Ramamoorthy, P (1988) Validation of a NASA code for determining the viscous supersonic flow past a pointed body of revolution. Technical Report. National Aeronautical Laboratory, Bangalore, India. GGopinath, PR and Sundaram, S and Madhavan, KT and Siddalingappa, SR and Yajnik, KS (1988) Flow visualisation of leading edge vortices on a Delta Wing by laser sheet technique. Technical Report. National Aeronautical Laboratory, Bangalore, India. KKannan, SM and Purohit, SC and Subramanian, NR (1988) Algebraic grid generation for missile-type configurations. Technical Report. National Aeronautical Laboratory, Bangalore, India. Kumar, Anand and Kumar, Senthil (1988) A new approach to grid generation based on local optimisation. In: 2nd International Conference of Numerical grid generation in computational fluid mechanics, 5-8 Dec.1988, Miami Beach,FL United Kingdom. MMathur, NB and Sreekanth, AK (1988) Separated transonic interaction characterstics of an afterbody configuration in presence of a central propulsive jet. Technical Report. National Aeronautical Laboratory, Bangalore,India. NNarasimha, R (1988) Introduction to irreducible tensor methods, Part 1. Technical Report. National Aeronautical Laboratory, Bangalore, India. Narasimha, Roddam and Das, P (1988) A spectral solution of the Boltzmann equation for the infinitely strong shock. Technical Report. National Aeronautical Laboratory, Bangalore, India. Nirmala, GA and Ramamoorthy, P (1988) NCSU Code for the determination of airloads on a Light Aircraft Fuselage and its application to LCRA. Technical Report. National Aeronautical Laboratory, Bangalore, India. RRamamoorthy, P (1988) A new method for designing natural laminar flow airfoils. Technical Report. National Aeronautical Laboratory, Bangalore, India. Ramamoorthy, P and Ramesh, S (1988) Design of a natural laminar flow airfoil (NAL-NLF-17O)for general aviation application. Technical Report. National Aeronautical Laboratory, Bangalore, India. SSengupta, TK and Selvarajan, S (1988) Study of flow past a circular cylinder using a higher order scheme for navier-stokes equation. Technical Report. National Aeronautical Laboratory, Bangalore,India. Shankar, PN (1988) Liquid-Vapour Phase change between plane liquid surfaces: A continuum analysis to determine real gas effects. Technical Report. National Aeronautical Laboratory, Bangalore, India. Shankar, PN and Deshpande, MD (1988) Experiments on liquid-vapour phase change between plane liquid surfaces Part I: experiments with water, freon and mercury. Technical Report. National Aeronautical Laboratory, Bangalore, India. Srilatha, KR and Ramamoorthy, P (1988) Allen's code for airfoil analysis. Technical Report. National Aeronautical Laboratory, Bangalore, India. Sundaram, S (1988) Skin friction measurements in a turbulent boundary layer. Technical Report. National Aeronautical Laboratory, Bangalore, India. YYajnik, KS and Sundaram, S and Sivaram, R (1988) Evaluation of drag reduction by turbulence control devices 13; 13;. In: IUTAM Symposium on turbulence management and relaminarisation, 13-23 Jan 1987, Bangalore, India. |