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Jump to: C | D | G | K | M | N | P | R | S | V
Number of items: 35.

C

Chandra, Ramesh and Guruprasad, K and Dwarakanath, K (1988) Energy release rates in patched cracked plates. Engineering Fracture Mechanics, 31 (5). pp. 719-732. ISSN 0013-7944

D

Desai, SS and Ragarajan, R and Singh, JP and Ravichandran, KS (1988) Full-potential calculations using Cartesian grids. Aeronautical Society of India, Journal, Vol. 4 . pp. 97-103.

Desai, SS and Rangarajan, R (1988) Mathematical modelling and computer simulation using cartesian grid. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Dutt, HNV (1988) Comment on 'Computation of the potential flow over airfoils with cusped or thin trailing edges'. AIAA Journal, 26 (1). pp. 122-123. ISSN 0001-1452

G

Gopinath, N and Narayan, KY (1988) Wind tunnel tests on LCA stage 4 configuration. Project Report. National Aerospace Laboratories, Bangalore.

K

Kanagarajan, V and Hartmann, K (1988) Force Measurements on a Body wing tail configuration (KaHa Model) at Mach numbers of 0.4 , 0.6 and 0.8 and incidences from 30° to 65°. Project Report. National Aerospace Laboratories, Bangalore.

M

Mathur, JS and Srinivasa, C (1988) Solution of a second order ODE by a multigrid method. Technical Report. National Aeronautical Laboratory, Bangalore, India.

N

Nagarajan, V and Sundara Murthy, H (1988) Estimation of stability derivatives and dynamic stability characteristics of basic and AEW HS-748 aircraft. Project Report. National Aerospace Laboratories, Bangalore.

Nanjundiah, Ravi S (1988) Simulation of Monsoon on Flosolver. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Narayan, G (1988) Augmentation of instrumentation systems for 1.2m tunnel. Project Report. National Aerospace Laboratories, Bangalore.

Narayan, KY (1988) Effect of Canard on the Characteristics of a 65° Delta Wing-A Preliminary Analysis of Experimental Data. Project Report. National Aerospace Laboratories, Bangalore.

Narayan, KY and Gopinath, N and Seshagiri, SN (1988) Wind tunnel tests on LCA 6.12 configuration. Project Report. National Aerospace Laboratories, Bangalore.

Narayan, KY and Hartmann, K (1988) Transonic and supersonic flow past a 65xB0; delta wing with rounded leading edges - analysis of experimental data. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Narayan, KY and Seshadri, SN (1988) Vortical flows on the lee surface of delta wings. Technical Report. National Aeronautical Laboratory, Bangalore, India.

P

Patil, SR and Ramaswamy, MA (1988) Development of Experimental Techniques to determine the Aerodynamic Performance of Helicopter Rotors in Hover and Forward Flight - Closure Report for AR & DB Project AE-0-154. Project Report. National Aerospace Laboratories, Bangalore.

Patil, SR and Ramaswamy, MA (1988) Development of experimental techniques for helicopter rotor performance studies. Aeronautical Society of India, Vol. 4 (3). pp. 201-209.

R

Radhakrishna, SR and Joseph, KA (1988) Regauging of internal strain gauge balance supplied by T.E.M limited to H.A.L., bangalore engineering. Project Report. National Aerospace Laboratories, Bangalore.

Rajagopalan, S (1988) Base-exchange softener and cooling water system - Chemical treatment and method of (control) testing of water. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Rajeswari, B and Dutt, HNV (1988) Analysis of wing flap configurations by a nonplanar vortex lattice method. Journal of Aircraft, 25 (2). pp. 97-98. ISSN 0021-8669

Ravichandran, KS and Rangarajan, R and Desai, SS and George, KP (1988) Vortex simulation in full potential solver on a cartesian grid. Technical Report. National Aeronautical Laboratory, Bangalore,India.

S

Selvarajan, S and Arokkiaswamy, A and Kanagarajan, V (1988) Wind Tunnel Force Measurements on 1/12 Scale Model of PRITHVI missile Configuration - II : Final Report. Project Report. National Aerospace Laboratories, Bangalore.

Sengupta, 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.

Seshadri, SN and Narayan, KY (1988) Possible types of flow on lee-surface of delta wings at supersonic speeds. Aeronautical Journal, 92 . pp. 185-199. ISSN 0001-9240

Singh, JP and Rangarajan, R and Desai, SS (1988) On the assessment of quot;Correctabilityquot; of data in two-dimensional transonic wind tunnel tests. Technical Report. National Aeronautical Laboratory, Bangalor, India.

Singh, JP and Rangarajan, R and Ramaswamy, MA (1988) Computation of flow over airfoils under high lift separated flow condition 13; 13;. Journal of Aeronautical Society of India, 40 . pp. 105-110.

Sinha, UN and Deshpande, MD and Sarasamma, VR (1988) Flosolver: A parallel computer for fluid dynamics. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Sinha, UN and Sarasamma, VR (1988) An iterative scheme for numerical solution of transonic small perturbation equation. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Sinha, UN and Sarasamma, VR and Sreenivasan, CR and Sivaramakrishnan, Rajalakshmy and Shridhar, N (1988) Sequential and parallelised version of transonic small perturbation code on flosolver. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Sreenivasan, CR (1988) Monitor program on programmable read only memories for Flosolver Mk1A. Project Report. National Aerospace Laboratories, Bangalore.

Sreenivasan, Sheila and Srikantan, KV (1988) Additional channel data acquisition through analogue tape recorder. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Srikantan, KV (1988) Additional standard wind tunnel balances for NTAF complex. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Srikantan, KV and Nirmala, GV (1988) Instrumentation for unsteady pressure measurement on cone cylinder configuration in NAL 1.2m Trisonic Wind 13; Tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Suryanarayana, BG (1988) Effect of ASB-II bombs and 800 litre drop tank on the aerodynamic characteristics of MiG-21 (M) aircraft. Project Report. National Aerospace Laboratories, Bangalore.

Swamy, Shivakumara M (1988) Wind tunnel testing of high blockage models. Journal of Aeronautical Society of India, 40 . pp. 119-130.

V

Viswanath, PR and Patil, SR (1988) Performance of passive devices for axisymmetric base drag reduction at mach 2. Technical Report. National Aeronautical Laboratory, Bangalore, India.

This list was generated on Thu Nov 27 01:16:37 2014 IST.