Organizational Unit:

Daniel Guggenheim School of Aerospace Engineering

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https://hdl.handle.net/1853/70742

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College of Engineering

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Aerospace Design Group

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Aerospace Systems Design Laboratory (ASDL)

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Air Transportation Laboratory

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Cognitive Engineering Center

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Space Systems Design Laboratory (SSDL)

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https://finding-aids.library.gatech.edu/agents/corporate_entities/106

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Assessment of the accuracy of existing real-time wake vortex models

2011-03-31 , Sankar, Lakshmi N. , Schrage, Daniel P. , Feigh, Karen M. , Huff, Brian , Flick, Ashley , Manivannan, Vasu

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Item

New approaches to HSCT multidisciplinary design and optimization

1999 , Schrage, Daniel P.

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Item

Study of the effects of rotating frame turbulence (RFT) on helicopter flight mechanics, loads, and vibration

1987 , Schrage, Daniel P. , Prasad, Jonnalagadda V. R.

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Helicopter stability and control modeling improvements and verification on two helicopters

1986 , Schrage, Daniel P.

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Item

Application of Georgia Tech generic IPPD methodology to support implementation of the NASA/Industry phase IIA propulsion plan high speed research program

1999 , Schrage, Daniel P.

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The assessment of capabilities and limitations of the flight lab simulation software in the prediction of rotorcraft component loads to support flight testing

1995 , Schrage, Daniel P.

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Turbulence model development for rotocraft stability and control specification

1987 , Schrage, Daniel P.

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NASA MDA Fellowship program (years 2-3)

1999 , Schrage, Daniel P.

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Development and evaluation of performance and handling qualities for low cost real time rotorcraft simulators-Phase I methodology development

1990 , Schrage, Daniel P. , Prasad, Jonnalagadda V. R.

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Item

Development of an individual blade control (IBC) computer analysis

1987 , Schrage, Daniel P.

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Organizational Unit:

Daniel Guggenheim School of Aerospace Engineering

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Assessment of the accuracy of existing real-time wake vortex models

New approaches to HSCT multidisciplinary design and optimization

Study of the effects of rotating frame turbulence (RFT) on helicopter flight mechanics, loads, and vibration

Helicopter stability and control modeling improvements and verification on two helicopters

Application of Georgia Tech generic IPPD methodology to support implementation of the NASA/Industry phase IIA propulsion plan high speed research program

The assessment of capabilities and limitations of the flight lab simulation software in the prediction of rotorcraft component loads to support flight testing

Turbulence model development for rotocraft stability and control specification

NASA MDA Fellowship program (years 2-3)

Development and evaluation of performance and handling qualities for low cost real time rotorcraft simulators-Phase I methodology development

Development of an individual blade control (IBC) computer analysis

Georgia Tech Library

Organizational Unit: Daniel Guggenheim School of Aerospace Engineering

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Publication Search Results

Assessment of the accuracy of existing real-time wake vortex models

New approaches to HSCT multidisciplinary design and optimization

Study of the effects of rotating frame turbulence (RFT) on helicopter flight mechanics, loads, and vibration

Helicopter stability and control modeling improvements and verification on two helicopters

Application of Georgia Tech generic IPPD methodology to support implementation of the NASA/Industry phase IIA propulsion plan high speed research program

The assessment of capabilities and limitations of the flight lab simulation software in the prediction of rotorcraft component loads to support flight testing

Turbulence model development for rotocraft stability and control specification

NASA MDA Fellowship program (years 2-3)

Development and evaluation of performance and handling qualities for low cost real time rotorcraft simulators-Phase I methodology development

Development of an individual blade control (IBC) computer analysis

Organizational Unit:

Daniel Guggenheim School of Aerospace Engineering