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title: aiaa scitech 2040 forum

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    Flutter Analysis with Stabilized Finite Elements Based on the Linearized Frequency-Domain Approach

    Kevin E Jacobson / Bret K Stanford / Stephen L Wood et al. | NTRS | 2020

    Airborne Science Mission Capabilities of the NASA DC-8 and Possible Alternative Aircraft

    Thomas A Ozoroski / James W Fenbert / Nicholas K Borer et al. | NTRS | 2020

    OSIRIS-REx Proximity Operations and Navigation Performanceat (101955) Bennu

    Peter G. Antreasian / Coralie D. Adam / Jeroen Geeraet et al. | NTRS | 2021
    pristine surface regolith were collected on October 20, 2020, when the OSIRIS-REx spacecraft successfully executed the Touch and Go (TAG) sample ...

    Autonomous Real-Time Global Aerodynamic Modeling in the Frequency Domain

    Eugene A Morelli | NTRS | 2020

    An Overview of NASA’s Learn-to-Fly Technology Development

    Stephen E Riddick | NTRS | 2020

    Training Astronauts using Hardware-in-the-Loop Simulations and Virtual Reality

    Angelica D. Garcia / Jonathan Schlueter / Eddie Paddock | NTRS

    Advances in Low-Cost Manufacturing and Folding of Solar Sail Membrane

    Olive R Stohlman / Juan M Fernandez / Gregory D Dean et al. | NTRS

    Human-in-the-Loop Flight Simulation Experiment on Unmanned Aircraft Terminal Operations

    Devin Patrick Jack / Keith D Hoffler / Roy D Roper et al. | NTRS

    A Simulation Framework for Precision Landing and Hazard Avoidance Technology Assessments

    Alicia Dwyer Cianciolo / Soumyo Dutta / Rafael Lugo et al. | NTRS | 2020

    InSight Entry, Descent and Landing Pre-Flight Performance Predictions

    Robert W Maddock / Alicia M Dwyer Cianciolo / Daniel K Litton et al. | NTRS | 2020

    Model Design and Pre-Test CFD Analysis for a Supersonic Retropropulsion Wind Tunnel Test

    Karl T Edquist / Ashley M Korzun / Bill Kleb et al. | NTRS | 2020
    . To that end, a retropropulsion wind tunnel test will be conducted in the NASA Langley Unitary Plan Wind Tunnel in 2020. The test is designed ...

    FLEET Velocimetry in the Common Research Model’s Wing Wake

    Daniel T Reese / Paul M Danehy / Eric L Walker et al. | NTRS | 2020

    Enabling Global Lunar Access for Human Landing Systems Staged at Earth-Moon L2 Southern Near Rectilinear Halo and Butterfly Orbits

    Zachary D May / Min Qu / Raymond G Merrill | NTRS | 2020

    Navigation Doppler Lidar Performance at High Speed and Long Range

    Aram Gragossian / Diego Pierrottet / Jay Estes et al. | NTRS

    InSight Entry, Descent and Landing Post-Flight Performance Assessment

    Robert W Maddock / Alicia M Dwyer Cianciolo / Ashley M Korzun et al. | NTRS | 2020

    Multi-Objective Flight Control for Ride Quality Improvement for Flexible Aircraft

    Nguyen, Nhan / Hashemi, Kelley | NTRS | 2020

    Design Factors for Two-Dimensional, External-Compression Supersonic Inlets

    Slater, John W. | NTRS | 2020

    Aeroheating Measurements of BOLT Aerodynamic Fairings and Transition Module

    Rieken, Elizabeth F. / Berry, Scott A. / Broslawski, Casey J. et al. | NTRS | 2020

    Computational Investigation of Powered Descent for Human-Scale Mars Landers

    Ashley M Korzun / Karen L Bibb / Francisco Canabal et al. | NTRS | 2020

    Jet Noise Prediction Comparisons with Scale Model Tests and Learjet Flyover Data

    Henderson, Brenda / Huff, Dennis / Berton, Jeff | NTRS | 2020

    Pterodactyl: The Development and Performance of Guidance Algorithms for a Mechanically Deployed Entry Vehicle

    Johnson, Breanna J. / Rocca-Bejar, Daniela / Lu, Ping et al. | NTRS | 2020

    Development of an Aeroservoelastic Model for Gust Load Alleviation of the NASA Common Research Model Wind Tunnel Experiment

    Cramer, Nick / Nguyen, Nhan | NTRS | 2020

    Supersonic Technology Concept Aeroplanes for Environmental Studies

    Berton, Jeffrey J. / Huff, Dennis L. / Seidel, Jonathan A. et al. | NTRS | 2020

    Adaptive Hexapod Simulator Motion Based on Aircraft Stability

    Zaal, Peter M. T. / Popovici, Alexandru / Lewis, Emily K. | NTRS | 2020

    Artificial Thickening of a Transonic Boundary Layer in the Presence of a Pressure Gradient Associated with a Boundary Layer Ingestion Concept

    Gregory S Jones / William Milholen / Alaa Elmiligui et al. | NTRS | 2020

    Fit2Fly: A Proof of Concept for Testing the Commercial Feasibility of Unmanned Aerial System Operations

    Ryan Bonk / Ryan Bowers / Samuel Buckner et al. | NTRS | 2020

    Mode-Based Sensing and Actuation Techniques for Multi-Objective Flexible Aircraft Control

    Hashemi, Kelley E. / Alder, Andrew / Cramer, Nick et al. | NTRS | 2020

    Evaluation of Low Cost, User-Centered Alerting Devices for the Mitigation of Flight Crew Spatial Disorientation

    Ronald J Daiker / Kathryn Ballard / Kyle K Ellis | NTRS | 2020

    Structural Analysis of Wind Tunnel Blades for the National Transonic Facility

    Brian H Mason / Andrew E Lovejoy / Daniel C Munden | NTRS | 2020

    Implementation of Acceleration Source Term in FUN3D

    Nash’at N Ahmad / Jan-Renee Carlson / Craig Streett et al. | NTRS | 2020

    ASPIRE Parachute Modeling and Comparison to Post-Flight Reconstruction

    Soumyo Dutta | NTRS | 2020
    2020 mission parachute. Prior to all three flights, a multi-body flight dynamics simulation was developed to predict the parachute dynamics and ...

    Hybrid Flush and Synthetic Air Data Filter for Entry Vehicle Atmospheric State Estimation

    Christopher D. Karlgaard | NTRS
    differences between the pressure and aerodynamic data sources. The filter is applied to data acquired during the Mars Science Laboratory and Mars 2020 ...

    Mars Helicopter Technology Demonstrator

    Balaram, J. (Bob) / Canham, Timothy / Duncan, Courtney et al. | NTRS | 2018
    . Much like the Sojourner rover on the Pathfinder mission paved the way for the Spirit, Opportunity, Curiosity and the Mars 2020 rovers, an ...

    Assessment of the Performance Potential of Advanced Subsonic Transport Concepts for NASA's Environmentally Responsible Aviation Project

    Nickol, Craig L. / Haller, William J. | NTRS | 2016
    ) of 4-6 by 2020. Progress towards this fuel burn reduction target was measured through the conceptual design and analysis of advanced subsonic ...

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