1–20 of 85 hits
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    AIR INTAKES AND EJECTORS

    Defence Research & Development Laboratory / Gas Turbine Research Establishment / National Aerospace Laboratories | British Library Conference Proceedings | 2000

    Hypersonic air breathing propulsion development - why, how and who?

    Prahlada / Defence Research & Development Laboratory / Gas Turbine Research Establishment et al. | British Library Conference Proceedings | 2000

    Air breathing propulsion system for hypersonic flight

    Shanker, V. / Defence Research & Development Laboratory / Gas Turbine Research Establishment et al. | British Library Conference Proceedings | 2000

    Air-breathing, self-refuelling propulsion systems: key to design of single-stage-to-orbit hypersonic aerospaceplanes

    Gopalaswami, R. / Defence Research & Development Laboratory / Gas Turbine Research Establishment et al. | British Library Conference Proceedings | 2000

    Solid - fuel ramjet assisted gun - launched projectile; an overview

    Krishnan, S. / Defence Research & Development Laboratory / Gas Turbine Research Establishment et al. | British Library Conference Proceedings | 2000

    Space launch vehicle propulsion - where are we and which way should we head?

    Nagappa, R. / Defence Research & Development Laboratory / Gas Turbine Research Establishment et al. | British Library Conference Proceedings | 2000

    Evaluation of cant/skew angle and thrust axis misalignment of booster sustainer propulsion system of typical ATGM on gantry CNC CMM

    Prasad, B. H. / Defence Research & Development Laboratory / Gas Turbine Research Establishment et al. | British Library Conference Proceedings | 2000

    Design experiences in interfacing Kaveri engine with TU-16 FTB for on board flight evaluation

    Shankar, M. R. / Defence Research & Development Laboratory / Gas Turbine Research Establishment et al. | British Library Conference Proceedings | 2000

    Some comments on control volume fuel element methods for fluid flow and heat transfer

    Baliga, B. R. / Defence Research & Development Laboratory / Gas Turbine Research Establishment et al. | British Library Conference Proceedings | 2000

    Ramjet and scramjet technologies: Focus at the National Aerospace Laboratories

    Prahlad, T. S. / Defence Research & Development Laboratory / Gas Turbine Research Establishment et al. | British Library Conference Proceedings | 2000

    Role combustion in propulsion - are there new frontiers to Conquer?

    Mukunda, H. S. / Defence Research & Development Laboratory / Gas Turbine Research Establishment et al. | British Library Conference Proceedings | 2000

    Some aspects on the leading edge swept sidewall compression scramjet inlet

    Thiagarajan, V. / Panneerselvam, S. / Defence Research & Development Laboratory et al. | British Library Conference Proceedings | 2000

    Performance improvement of a low aspect ratio axial flow compressor rotor by means of turbulence generator

    Sitaram, N. / Thakar, R. / Defence Research & Development Laboratory et al. | British Library Conference Proceedings | 2000

    Residual life estimation of critical aero engine components

    Kishan / Ippili, S. R. / Defence Research & Development Laboratory et al. | British Library Conference Proceedings | 2000

    High energy high density liquid fuels for ramjet/scramjet propulsion

    Singh, R. V. / Krishnamachary, S. / Defence Research & Development Laboratory et al. | British Library Conference Proceedings | 2000

    Experimental investigations on ignition of AP-HTPB sandwich propellants

    Sridhar, B. T. / Padmanabham, G. / Defence Research & Development Laboratory et al. | British Library Conference Proceedings | 2000

    Investigations of effect of blade trailing edge ejection on the aerodynamic performance in case of a turbine cascade

    Manickam, M. D. / Murugesan, K. / Defence Research & Development Laboratory et al. | British Library Conference Proceedings | 2000

    Prediction of the recirculation zone in supersonic combustor

    Sinha, P. K. / Anandanarayana, K. / Defence Research & Development Laboratory et al. | British Library Conference Proceedings | 2000

    Multigrid solution of the shock boundary layer interaction problem

    Durga, K. K. / Ramakrishna, M. / Defence Research & Development Laboratory et al. | British Library Conference Proceedings | 2000

    A computational study of a three dimensional sidewall suppression inlet for a scramjet engine

    Singh, A. / Sen, P. K. / Defence Research & Development Laboratory et al. | British Library Conference Proceedings | 2000