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Dev G Rajnarayan

from Mountain View, CA
Age ~45

Dev Rajnarayan Phones & Addresses

  • 439 Beaume Ct, Mountain View, CA 94043
  • Stanford, CA

Work

Company: Aerion corporation May 2018 Position: Chief software architect

Education

School / High School: Stanford University 2005 to 2009

Skills

Machine Learning • Algorithms • Matlab • Optimization • Aerodynamics • Scientific Computing • C • Robotics • Embedded Systems • Numerical Analysis • Modeling • Cfd • Fluid Dynamics • Applied Mathematics • Simulations • Mechatronics • Java • Fortran • Optimizations • Numerical Modeling

Languages

English

Interests

Science and Technology

Industries

Airlines/Aviation

Professional Records

License Records

Dev Gorur Rajnarayan

Address:
439 Beaume Ct, Mountain View, CA 94043
License #:
A4928712
Category:
Airmen

Resumes

Resumes

Dev Rajnarayan Photo 1

Chief Software Architect

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Location:
Palo Alto, CA
Industry:
Airlines/Aviation
Work:
Aerion Corporation
Chief Software Architect

Aerion Corporation Oct 2017 - May 2018
Software Architect

Aerion Corporation Jul 2013 - Oct 2017
Senior Design Engineer

Sensor Platforms May 2012 - Jul 2013
Algorithms Engineer

Desktop Aeronautics 2009 - May 2012
Engineer
Education:
Stanford University 2005 - 2009
Stanford University 2003 - 2005
Master of Science, Masters
Indian Institute of Technology, Bombay 1998 - 2002
Skills:
Machine Learning
Algorithms
Matlab
Optimization
Aerodynamics
Scientific Computing
C
Robotics
Embedded Systems
Numerical Analysis
Modeling
Cfd
Fluid Dynamics
Applied Mathematics
Simulations
Mechatronics
Java
Fortran
Optimizations
Numerical Modeling
Interests:
Science and Technology
Languages:
English

Publications

Us Patents

Predicting Transition From Laminar To Turbulent Flow Over A Surface

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US Patent:
20120245910, Sep 27, 2012
Filed:
Mar 22, 2011
Appl. No.:
13/069374
Inventors:
Dev RAJNARAYAN - Mountain View CA, US
Peter Sturdza - Redwood City CA, US
Assignee:
DESKTOP AERONAUTICS, INC. - Palo Alto CA
International Classification:
G06G 7/57
US Classification:
703 9
Abstract:
A prediction of whether a point on a computer-generated surface is adjacent to laminar or turbulent flow is made using a transition prediction technique. A plurality of boundary-layer properties at the point are obtained from a steady-state solution of a fluid flow in a region adjacent to the point. A plurality of instability modes are obtained, each defined by one or more mode parameters. A vector of regressor weights is obtained for the known instability growth rates in a training dataset. For each instability mode in the plurality of instability modes, a covariance vector is determined, which is the covariance of a predicted local growth rate with the known instability growth rates. Each covariance vector is used with the vector of regressor weights to determine a predicted local growth rate at the point. Based on the predicted local growth rates, an n-factor envelope at the point is determined.

Predicting Transition From Laminar To Turbulent Flow Over A Surface Using Mode-Shape Parameters

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US Patent:
20130282629, Oct 24, 2013
Filed:
Mar 26, 2013
Appl. No.:
13/850628
Inventors:
Dev Rajnarayan - Mountain View CA, US
Peter Sturdza - Redwood City CA, US
Assignee:
AERION CORPORATION - Reno NV
International Classification:
G06F 17/50
G06N 99/00
US Classification:
706 12
Abstract:
In accordance with embodiments disclosed herein, there are provided methods, systems, and apparatuses for predicting whether a point on a computer-generated aircraft or vehicle surface is adjacent to laminar or turbulent flow is made using a transition prediction technique. A plurality of boundary-layer properties at the point are obtained from a steady-state solution of a fluid flow in a region adjacent to the point. Included in the list of boundary-layer properties are computed coefficients or weights of mode shapes that describe the boundary-layer profiles. A plurality of instability modes are obtained, each defined by one or more mode parameters. A vector of regressor weights is obtained for the known instability growth rates in a training dataset. For each instability mode in the plurality of instability modes, a covariance vector is determined, which is the covariance of a predicted local growth rate with the known instability growth rates. Each covariance vector is used with the vector of regressor weights to determine a predicted local growth rate at the point. Based on the predicted local growth rates, an n-factor envelope at the point is determined.

Computing Techniques For Three-Dimensional Modeling And Design Analysis

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US Patent:
20220300673, Sep 22, 2022
Filed:
Feb 9, 2022
Appl. No.:
17/668222
Inventors:
Joseph J. Luzinski - Fort Lauderdale FL, US
Bharath Mukundakrishnan - San Jose CA, US
Sushrut S. Pavanaskar - Castro Valley CA, US
Dev G. Rajnarayan - Mountain View CA, US
International Classification:
G06F 30/15
B64F 5/00
G06F 30/20
Abstract:
Techniques and systems for creating and performing analysis on three-dimensional computer models are described. The model creation and analysis may be specified using an un-compiled script that includes a set of instructions. The set of instructions may implement a computer-aided design (CAD) kernel using a bridge layer that includes compiled bridge code. The instructions may be used to create a job set having a group of tasks. Using the job set, a processing queue may be constructed, the processing queue having a subset of common tasks prioritized within the processing queue. Subsets or groups of tasks or instructions may also be executed in parallel using multiple distinct processors or a multi-threaded processor.

Computing Techniques For Three-Dimensional Modeling And Design Analysis

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US Patent:
20190005185, Jan 3, 2019
Filed:
Jun 29, 2018
Appl. No.:
16/023162
Inventors:
- Reno NV, US
Bharath Mukundakrishnan - San Jose CA, US
Sushrut S. Pavanaskar - Castro Valley CA, US
Dev G. Rajnarayan - Mountain View CA, US
International Classification:
G06F 17/50
B64F 5/00
Abstract:
Techniques and systems for creating and performing analysis on three-dimensional computer models are described. The model creation and analysis may be specified using an un-compiled script that includes a set of instructions. The set of instructions may implement a computer-aided design (CAD) kernel using a bridge layer that includes compiled bridge code. The instructions may be used to create a job set having a group of tasks. Using the job set, a processing queue may be constructed, the processing queue having a subset of common tasks prioritized within the processing queue. Subsets or groups of tasks or instructions may also be executed in parallel using multiple distinct processors or a multi-threaded processor.

Solid Modeler That Provides Spatial Gradients Of 3D Cad Models Of Solid Objects

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US Patent:
20180293792, Oct 11, 2018
Filed:
Apr 5, 2018
Appl. No.:
15/946572
Inventors:
- Reno NV, US
Bharath Mukundakrishnan - San Jose CA, US
Raymond P. D'Antuono - El Cerrito CA, US
Dev G. Rajnarayan - Mountain View CA, US
International Classification:
G06T 17/20
G06T 15/50
G06T 15/04
G06T 19/20
G06F 17/30
Abstract:
This disclosure provides a method for providing spatial gradients of 3D CAD models of solid objects with respect to various parameters used in defining the solid object. A modeler is designed and implemented to provide spatial gradients of solid objects (when represented on a computer as 3D CAD models) with respect to the various parameters that define the objects. Although primarily based on finite difference operations, several additional steps are performed to ensure that the gradients computed are correct and valid for a general class of solid objects and the parameters that define the objects. No commercially available 3D CAD tool provides such ability for a general class of solid objects.

Predicting Transition From Laminar To Turbulent Flow Over A Surface Using Mode-Shape Parameters

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US Patent:
20170045417, Feb 16, 2017
Filed:
Oct 26, 2016
Appl. No.:
15/335303
Inventors:
Dev Rajnarayan - Mountain View CA, US
Peter Sturdza - Redwood City CA, US
Assignee:
Aerion Corporation - Reno NV
International Classification:
G01M 9/06
G06F 17/50
G01M 9/08
Abstract:
In accordance with embodiments disclosed herein, there are provided methods, systems, and apparatuses for predicting whether a point on a computer-generated aircraft or vehicle surface is adjacent to laminar or turbulent flow is made using a transition prediction technique. A plurality of boundary-layer properties at the point are obtained from a steady-state solution of a fluid flow in a region adjacent to the point. Included in the list of boundary-layer properties are computed coefficients or weights of mode shapes that describe the boundary-layer profiles. A plurality of instability modes are obtained, each defined by one or more mode parameters. A vector of regressor weights is obtained for the known instability growth rates in a training dataset. For each instability mode in the plurality of instability modes, a covariance vector is determined, which is the covariance of a predicted local growth rate with the known instability growth rates. Each covariance vector is used with the vector of regressor weights to determine a predicted local growth rate at the point. Based on the predicted local growth rates, an n-factor envelope at the point is determined.

Selecting Feature Types To Extract Based On Pre-Classification Of Sensor Measurements

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US Patent:
20150012248, Jan 8, 2015
Filed:
Jul 1, 2014
Appl. No.:
14/321707
Inventors:
- San Jose CA, US
Tom Waite - El Sobrante CA, US
Dev Rajnarayan - Mountain View CA, US
International Classification:
G06F 3/01
US Classification:
702189
Abstract:
A processing apparatus including one or more processors and memory receives sensor measurements generated by one or more sensors of one or more devices, pre-classifies the sensor measurements as belonging to one of a plurality of pre-classifications, and selects one or more feature types to extract from the sensor measurements based at least in part on the pre-classification of the sensor measurements. The processing apparatus also extracts features of the one or more selected feature types from the sensor measurements and determines a state of a respective device of the one or more devices in accordance with a classification of the sensor measurements determined based on the one or more features extracted from the sensor measurements.

Combining Monitoring Sensor Measurements And System Signals To Determine Device Context

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US Patent:
20140149060, May 29, 2014
Filed:
Nov 26, 2013
Appl. No.:
14/090966
Inventors:
- San Jose CA, US
Dev Rajnarayan - Mountain View CA, US
James V. Steele - Los Gatos CA, US
Ian Chen - Campbell CA, US
Assignee:
Sensor Platforms, Inc. - San Jose CA
International Classification:
G01C 25/00
US Classification:
702 94
Abstract:
A processing apparatus including one or more processors and memory obtains one or more sensor measurements generated by one or more monitoring sensors of one or more devices, including one or more monitoring sensor measurements from a respective monitoring sensor of a respective device and obtains one or more system signals including a respective system signal corresponding to current operation of the respective device. The processing apparatus determines device context information for the respective device based on the one or more sensor measurements and the one or more system signals and adjusts operation of the device in accordance with the device context information.
Dev G Rajnarayan from Mountain View, CA, age ~45 Get Report