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Bera, Rajendra K (1989) An Accurate method for calculating the initial development of vortex sheets. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Bera, Rajendra K (1989) Design priorities for an air-superiority fighter. Journal of Aeronautical Society of India, 41. pp. 407-411.
Bera, Rajendra K (1989) Design priorities for an air-superiority fighter. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Bera, Rajendra K (1989) Developing fighter software. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Bera, Rajendra K (1989) Engineering education and training initiatives for the 1990s. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Bera, Rajendra K (1989) New look at Theodorsen's method in aerofoil theory. International Journal for Numerical Methods in Fluids, 9 (3). pp. 251-262. ISSN 0271-2091
Bera, Rajendra K (1989) On the dynamics of point vortices. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Bera, Rajendra K and Suresh, G (1989) Comments on the lawrence equation for low-aspect-ratio wings. Journal of Aircraft, 26 (9). pp. 883-885. ISSN 0021-8669
CTFD, - (1989) Illustrative results from typical software in the Computational and Theoretical Fluid Dynamics Division. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Chakrabartty, SK (1989) Computation of transonic potential flow RAE-wing-A and body-B2 combination. Technical Report. National Aeronautical Laboratory, Bangalore,India.
Chakrabartty, SK and Subramanian, NR (1989) Computation of 3-D transonic flows for wings and wing-body configurations (Closure Report)13;. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Chakrabartty, SK and Subramanian, NR (1989) Computation of 3-D transonic flows for wings and wing-body13; configurations (Annual Progress Report). Technical Report. National Aeronautical Laboratory, Bangalore, India.
Deshpande, MD and Shankar, PN (1989) Error analysis for liquid-vapour phase change experiments. Technical Report. National Aerospace Laboratories, Bangalore, India.
Deshpande, MD and Sreenivasan, CR and Sridhar, S and Sarasamma, VR (1989) Presentations at the Flosolver Workshop :27-28 December 1988. Project Report. National Aerospace Laboratories, Bangalore.
Dutta, PK (1989) Discrete vortex simulation of high reynolds number flows. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Dutta, Vimala (1989) An implicit navier-stokes solver for the steady laminar supersonic flow past a semi-infinite flat plate at zero incidence. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Govindarajan, Rama and Narasimha, R (1989) The role of residual non-turbulent disturbances on 13; transition onset in two-dimensional boundary layers. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Kumar, Anand (1989) Flow calculation over a delta-wing using the thin-layer wavier-stokes equations. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Kumar, Anand (1989) Flow-calculation over a delta-wing using the thin-layer Navier-Stokes equations. In: 3rd International Symposium on Computational Fluid Dynamics, 28-31 Aug 1989, Nagoya, Japan.
Narayana, CL and Dwarakanath, GS and Sinha, UN and Sarasamma, VR and Rajalakshmy, S and Sreenivasan, CR and Sridhar, S (1989) Preliminary report on the parallelisation of the panel code on Flosolver. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramamoorthy, P (1989) Extended Kalman Filter Algorithm (EKF). Technical Report. National Aerospace Laboratories, Bangalore, India.
Ramamoorthy, P and Chakravarthy, Rajesh R (1989) Solution of Blasius equation by Tchebychev Spectral Method. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Ramamoorthy, P and Prasad, SK (1989) Analysis and Design of Symmetrical Airfoils. Technical Report. National Aerospace Laboratories, Bangalore, India.
Sanjay, K (1989) Parallel algorithm for Euler equations (one and two dimensional) using kinetic fiyx vector splitting. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sanjay, K and Sinha, UN and Shankar, PN (1989) Laplace solver. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Singh, JP (1989) Computation of viscous axisymmetric transonic flow using cartesian grids. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Singh, JP (1989) Multigrid accelerated relaxation solution of transonic full potential flow equation. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Singh, JP (1989) Solution of laplace equation using full approximation storage multigrid technique. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sinha, UN (1989) Outline of the method of complex characteristics. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sinha, UN and Shankar, PN (1989) A Fast Poisson Solver in Two Dimensions. Technical Report. National Aerospace Laboratories, Bangalore, India.
Sreenivasan, CR and Sivaramakrishnan, Rajalakshmy and Sarasamma, VR (1989) Flosolver Mk1B - An eight processor parallel machine. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sridhar, S and Swamy, Kiran and Sinha, UN (1989) Extending I/O Capabilities to Processing Elements of Flosolver. Technical Report. National Aerospace Laboratories, Bangalore, India.
Srilatha, KR and Dwarakanath, GS and Ramamoorthy, P (1989) Design of NAL-NLF-208-MARK 2 airfoil for NAL's light aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Srilatha, KR and Dwarakanath, GS and Ramamoorthy, P (1989) Design of a natural laminar flow airfoil for NAL's light Aircraft. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Srilatha, KR and Ramamoorthy, P (1989) Performance of NAL- MSNLF-136 airfoil with boundary layer tripped at 5 and 10 of the chord. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Srivastava, Ashok (1989) Prediction of aerodynamic characteristics of wing body combinations at high angles of attack experience with an13; existing code. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Subramanian, NR and Kumar, Anand (1989) Role of Supercomputer in Computational Aerodynamics. Technical Report. National aerospace Laboratories, Bangalore,India.
Sundaravaradhan, G and Sinha, UN (1989) Implementation of synchronisation using Interrupts - I. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Sundaravaradhan, G and Sinha, UN (1989) Synchronous transmission using ATX 351. Technical Report. National Aeronautical Laboratory, Bangalore, India.
Varadhan, Sundara G and Sinha, UN (1989) Serial transfer between two nodes using synchronous mode. Technical Report. National Aeronautical Laboratory, Bangalore, India.
