Design and Development of Aerospace Vehicles and Propulsion Systems: Proceedings of SAROD 2018

529 Pages·2021·39.765 MB·English

by  S. Kishore Kumar, Indira Narayanaswamy, V. Ramesh

Lecture Notes in Mechanical Engineering
S. Kishore Kumar
Indira Narayanaswamy
V. Ramesh   Editors
Design and
Development
of Aerospace Vehicles
and Propulsion Systems
Proceedings of SAROD 2018
Lecture Notes in Mechanical Engineering
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Engineering, Graduate School of Engineering and Applied Science, Monterey,
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S. Kishore Kumar Indira Narayanaswamy
(cid:129) (cid:129)
V. Ramesh
Editors
Design and Development
of Aerospace Vehicles
and Propulsion Systems
Proceedings of SAROD 2018
123
Editors
S. KishoreKumar Indira Narayanaswamy
GasTurbine Research Establishment M.S. RamaiahUniversity of Applied
Bengaluru, Karnataka, India Sciences
Bengaluru, Karnataka, India
V.Ramesh
National Aerospace Laboratories
Bengaluru, Karnataka, India
ISSN 2195-4356 ISSN 2195-4364 (electronic)
Lecture Notesin MechanicalEngineering
ISBN978-981-15-9600-1 ISBN978-981-15-9601-8 (eBook)
https://doi.org/10.1007/978-981-15-9601-8
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Contents
MachNumberEffectonAeroacousticCharacteristicsofCompressible
Jet Due to Chevron . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
S. R. Nikam and S. D. Sharma
Parametric Study of Turbulent Flow Past a Compression–
Decompression Ramp. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15
Rhea George and Raj Kiran Grandhi
Validation of Numerical Analysis Results for Pusher Configured
Turboprop Engine Air Intake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25
C. A. Vinay and S. Bhaskar Chakravarthy
Aero-elastic Analysis of High Aspect Ratio UAV Wing—Based
on Two-Way Fluid Structure Interaction. . . . . . . . . . . . . . . . . . . . . . . . 37
Vidit Sharma and S. Keshava Kumar
Numerical Study of Effect of Adjacent Blades Oscillation
in a Compressor Cascade. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 59
Shubham, M. C. Keerthi, and Abhijit Kushari
Effect of Incoming Wakes on Losses of a Low-Pressure Turbine
of a Gas Turbine Engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75
Vishal Tandon, Gopalan Jagadeesh, and S. V. Ramana Murty
Effect of Axial Location on the Performance of a Control Jet
in a Supersonic Cross Flow . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 89
Raj Kiran Grandhi and Arnab Roy
Effect of Chord Variation on Subsonic Aerodynamics of Grid Fins. . . . 105
Manish Tripathi, Mahesh M. Sucheendran, and Ajay Misra
Numerical Investigation on the Effect of Propeller Slipstream
on the Performance of Wing at Low Reynolds Numbers . . . . . . . . . . . . 129
K. Shruti and M. Sivapragasam
v
vi Contents
Theoretical Design and Performance Evaluation of a Two-Ramp
and a Three-Ramp Rectangular Mixed Compression Intake
in the Mach Range of 2–4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 143
Subrat Partha Sarathi Pattnaik and N. K. S. Rajan
Sensitivity of Altitude Variation on Aerodynamics of a Typical
Launch Vehicle During Hot Separation . . . . . . . . . . . . . . . . . . . . . . . . . 167
Jiju R. Justus, Sanjoy Kumar Saha, and Pankaj Priyadarshi
Normal Shock Dynamics in Internal Supersonic Flows . . . . . . . . . . . . . 177
S. Vaisakh and T. M. Muruganandam
Hinge Moment Characterization of All Movable Control Surface . . . . . 185
Manoj Kumar, G. Kadam Sunil, V. Shanmugam, and G. Balu
3D Computational Studies of Flapping Wing in Frontal Gusty Shear
Flow. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 197
M. De Manabendra, J. S. Mathur, and S. Vengadesan
InvestigationofWindTunnelBlockageEffectonLiftoffAerodynamics
of a Launch Vehicle Through Open-Source CFD Solver SU2 . . . . . . . . 211
Aaditya N. Chaphalkar, Amit Sachdeva, Vinod Kumar,
and Pankaj Priyadarshi
Observation of Low-Frequency Shock Oscillation Over
a Forward-Facing Step. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 219
Jayaprakash N. Murugan and Raghuraman N. Govardhan
RANS Computations of Hypersonic Interference Heating on Flat
Surface with Protuberances . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 227
M. Mahendhran and C. Balaji
Multi-fidelity Aerodynamic Optimization of an Airfoil
at a Transitional Low Reynolds Number . . . . . . . . . . . . . . . . . . . . . . . . 239
R. Priyanka, M. Sivapragasam, and H. K. Narahari
Aerodynamic Optimization of Transonic Wing for Light
Jet Aircraft. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 253
K. Sathyandra Rao, M. Sivapragasam, H. K. Narahari,
and Aneash V. Bharadwaj
Non-adiabatic Wall Effects on Transonic Shock/Boundary Layer
Interaction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 267
Sahil Bhola and Tapan K. Sengupta
An Adjoint Approach for Accurate Shape Sensitivities in 3D
Compressible Flows . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 289
Srikanth Sathyanarayana, Anil Nemili, Ashish Bhole,
and Praveen Chandrashekar
Contents vii
Robust Flutter Prediction of an Airfoil Including Uncertainties. . . . . . . 305
A. Arun Kumar and Amit Kumar Onkar
Effect of Vortex Generator on Flow in a Serpentine Air Intake
Duct . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 315
B. B. Shivakumar, H. K. Narahari, and Padmanabhan Jayasimha
Supersonic Flow Behavior in Cartridge Starter . . . . . . . . . . . . . . . . . . . 331
Ritesh Gaur, Suparna Pal, Vimala Narayanan, D. Kishore Prasad,
and N. Balamurali Krishnan
High-Speed Shadowgraph Visualization Studies of the Effectiveness
of Ventilating a V-Gutter Flame Holder to Mitigate Screech
Combustion Instability in an Aero-Gas Turbine Afterburner . . . . . . . . 343
C. Rajashekar, Shambhoo, H. S. Raghukumar, R. M. Udaya Kumar,
K. Ashirvadam, and J. J. Isaac
Passive Reduction of Aerodynamic Rolling Moment for a Launch
Vehicle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 359
Pankaj Priyadarshi, Amit Sachdeva, and Leya Joseph
Design and Development of Miniature Mass Flow Control Unit
for Air-Intake Characterization . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 377
D. B. Singh, P. Vinay Raya, Buddhadeb Nath, N. Srinivasan,
Anju Sharma, and B. Sampath Rao
The Effect of Variable Inlet Guide Vanes on the Performance
of Military Engine Fan. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 387
Baljeet Kaur, Reza Abbas, and Ajay Pratap
Transition Prediction for Flow Over a MAV Wing Using
the Correlation Based Model . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 403
M. B. Subrahmanya and B. N. Rajani
RotorFlowAnalysisinthePresenceofFuselageUsingUnsteadyPanel
Method. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 415
K. R. Srilatha, Premalatha, and Vidyadhar Y. Mudkavi
Numerical Analysis of High Reynolds Number Effects
on the Performance of GAW-1 Airfoil . . . . . . . . . . . . . . . . . . . . . . . . . . 425
D. S. Kulkarni and B. N. Rajani
Investigation of the Effect of Booster Attachment Scheme
on the Rolling Moment Characteristics of an Asymmetric
Vehicle Using CFD. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 433
P. K. Sinha, Munish Kumar Ralh, Naveed Ali, R. Krishnamohan Rao,
and G. Balu
viii Contents
Multi-objective Optimization Approach for Low RCS Aerodynamic
Design of Aerospace Structures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 445
P. S. Shibu, Sandeep, Balamati Choudhury, and R. U. Nair
Analysis of Propeller by Panel Method for Transport Aircraft . . . . . . . 457
Premalatha, K. R. Srilatha, and Vidyadhar Y. Mudkavi
Effect of Reynolds Number on Typical Civil Transport Aircraft . . . . . . 471
Vishal S. Shirbhate, K. Siva Kumar, and K. Madhu Babu
Prediction of MultiStore Separation from a Fighter Aircraft
Using In-House Code—WISe . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 481
S. Karthik, Jishnu Suresh, P. Karthikeya, S. Rajkumar, Mano Prakash,
Sashi Kiran, and D. Narayan
Shockwave Oscillations Over the Conical Heat Shield Region
of a Typical Launch Vehicle at Mach 0.95. . . . . . . . . . . . . . . . . . . . . . . 491
K. N. Murugan, T. Arunkumar, M. Prasath, and V. R. Ganesan
Diverterless Supersonic Intake for a Generic Stealth Fighter
Aircraft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 501
Sameer Karania, Manu Mohan, and Satya Prakash
Analysis of Missile Plume Impact Characteristics on Engine Intake
and Neighboring Stores for a Fighter Aircraft. . . . . . . . . . . . . . . . . . . . 511
Jishnu Suresh, S. Karthik, P. Karthikeya, S. Rajkumar, Mano Prakash,
Sashi Kiran, D. Maharana, and D. Narayan
Control of Tailless Aircraft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 523
T. S. Ganesh, M. C. Keerthi, Sabari Girish, S. Sreeja Kumar,
and B. Mrunalini
About the Editors
Dr. S. Kishore Kumar is a DRDO fellow in the Gas and Turbine Research
Establishment (GTRE), Associate Editor of Journal of Aerospace Sciences &
Technologies of AeSI and Technical Adviser to National Design & Research
Forum. He has previously served as Associate Director and Programme Director
(GATET),GTRE.Hisareasofspecializationincludedesign&CFDanalysisofGas
Turbine Engines, Optimization, mathematical modelling and dynamical systems.
Hehaspublished7editedvolumesandmorethan100researchpapers&technical
reports.
Dr. Indira Narayanaswamy is a Research Professor at Ramaiah University of
Applied Sciences, Bangalore, India. She has previously served as a scientist and
Technology Director at Aeronautical Development Agency, Bangalore.
Dr. Narayanaswamy’s areas of specialization include CFD applications for
Aerodynamic Shape Optimization and Multidisciplinary Design Optimization
(MDO),MDOforMAVdesignandNumericalInvestigationsonSupersonicRetro
Propulsion (SRP). She has authored more than 150 research papers and technical
reports.SheisoneoftheEditorsoftheProceedingsofthe2ndNationalConference
on MDAO, published by Springer Nature Singapore Pte Ltd, 2020.
Dr.V.Ramesh istheheadoftheCTFDDivisioninNAL,anAcSIRProfessorand
theSecretaryoftheCFDDivisionoftheAeronauticsSocietyofIndia.Hisresearch
interests are primarily in aerospace science and technology, and includes
Computational Fluid Dynamics (CFD), mesh free methods, and computational
aero-elasticity. He has authored more than 150 research publications and reports.
ix