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The FAA conducts research to ensure that commercial and general aviation is the safest in the world. Bookmark this collection https://rosap.ntl.bts.gov/collection_faa or https://doi.org/10.21949/1530831.

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  • Analysis of Approach Stability and Challenges in Operational Implementation of RNP Approach Procedures
    Analysis of Approach Stability and Challenges in Operational Implementation of RNP Approach Procedures
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  • Rotorcraft Noise Abatement Operating Conditions Modeling
    Rotorcraft Noise Abatement Operating Conditions Modeling
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  • Effect of Distillate Fraction of Real Jet Fuel on Sooting Propensity  Part 1 Nascent Soot Formation in Premixed StretchStabilized Flames
    Effect of Distillate Fraction of Real Jet Fuel on Sooting Propensity – Part 1: Nascent Soot Formation in Premixed Stretch-Stabilized Flames
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  • Fuel Effects on Lean BlowOut in a Realistic Gas Turbine Combustor
    Fuel Effects on Lean Blow-Out in a Realistic Gas Turbine Combustor
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  • Modeling Performance and Noise of Advanced Operational Procedures for Current and Future Aircraft
    Modeling Performance and Noise of Advanced Operational Procedures for Current and Future Aircraft
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  • FAA Aerospace Forecast Fiscal Years 20172037
    FAA Aerospace Forecast: Fiscal Years 2017-2037
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  • Low Temperature Autoignition of Conventional Jet Fuels and Surrogate Jet Fuels With Targeted Properties in a Rapid Compression Machine
    Low Temperature Autoignition of Conventional Jet Fuels and Surrogate Jet Fuels With Targeted Properties in a Rapid Compression Machine
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  • Designing Flightdeck Procedures
    Designing Flightdeck Procedures
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  • FAA Center of Excellence Alternative Jet Fuels  Environment  Annual Technical Report 2016  For the Period October 1 2015  September 30 2016
    FAA Center of Excellence Alternative Jet Fuels & Environment : Annual Technical Report 2016 : For the Period October 1, 2015 - September 30, 2016
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  • Effects of Nocturnal Air and Rail Traffic Noise on Sleep
    Effects of Nocturnal Air and Rail Traffic Noise on Sleep
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  • TASOPT Engine Model Development A PARTNER Project 48 Report
    TASOPT Engine Model Development: A PARTNER Project 48 Report
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  • Two Laboratory Studies of Peoples Responses to Sonic Booms and Other Transient Sounds as Heard Indoors The PARTNER Project 24 Final Report
    Two Laboratory Studies of People’s Responses to Sonic Booms and Other Transient Sounds as Heard Indoors: The PARTNER Project 24 Final Report
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  • FAA Aerospace Forecast Fiscal Years 20162036
    FAA Aerospace Forecast: Fiscal Years 2016-2036
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  • FAA Center of Excellence for Alternative Jet Fuels  Environment  Annual Technical Report  December 2016  For the period September 13 2013  September 30 2015
    FAA Center of Excellence for Alternative Jet Fuels & Environment : Annual Technical Report : December, 2016 : For the period September 13, 2013 - September 30, 2015
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  • Cruise Fuel Reduction Potential from Altitude and Speed Optimization in Global Airline Operations
    Cruise Fuel Reduction Potential from Altitude and Speed Optimization in Global Airline Operations
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  • Aviation NOxInduced CH4 Effect Fixed Mixing Ratio Boundary Conditions Versus Flux Boundary Conditions
    Aviation NOx-Induced CH4 Effect: Fixed Mixing Ratio Boundary Conditions Versus Flux Boundary Conditions
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  • Alerts and Cues for Specific Conditions Analysis and Application in Training
    Alerts and Cues for Specific Conditions: Analysis and Application in Training
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  • FAA Aerospace Forecast Fiscal Years 20152035
    FAA Aerospace Forecast: Fiscal Years 2015-2035
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  • Flight Crew and Air Traffic Controller Interactions When Conducting Interval Management Utilizing Voice and Controller Pilot Data Link Communications
    Flight Crew and Air Traffic Controller Interactions When Conducting Interval Management Utilizing Voice and Controller Pilot Data Link Communications
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  • Calculation of Sensitivity Coefficients for Individual Airport Emissions in the Continental US Using CMAQDDMPM
    Calculation of Sensitivity Coefficients for Individual Airport Emissions in the Continental U.S. Using CMAQ-DDM/PM
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