aerospace-engineering

Documents about aerospace-engineering

• The influence of a model on plenum chamber indication of mach number in a slotted wall wind tunnel#491747AERADE
• The longitudinal response of an aircraft with auto-pilot, including an incidence term in the height control equation#491748AERADE
• F-Layer Parameters Derived by Airglow Emissions at Pituffik SB, Greenland#623762DigitalCommons@USU
• Cryogenic Gas Cell for Infrared Space Instrumentation#623774DigitalCommons@USU
• Generation and statistical validation of synthetic foamed concrete mix data using a Gaussian copula model#326454Iowa State University Digital Repository
• Energetic Characterization of 3-D Printed Acrylonitrile Butadiene Styrene Fuels for Hybrid Rocket Propulsion Applications#325538DigitalCommons@USU
• Graphics Processing Unit-Enabled Path Planning Based on Global Evolutionary Dynamic Programming and Local Genetic Algorithm Optimization#450523Scholar Commons
• Investigating Alternative Designs for Flow Fields and Porous Transport Layers in Proton Exchange Membrane Water Electrolyzers#996306eScholarship
• Concurrent Engineering Software Development at German Aerospace Center -Status and Outlook-#217559electronic library
• Low-speed tunnel investigation of the effect of the body on Cmo and aerodynamic centre of unswept wing-body combinations#491368AERADE
• Some curves for use in calculations of the performance of conical centrebody intakes at supersonic speeds and at full mass flow#491460AERADE
• Wake survey and straingauge measurements on an inclined propeller in the R.A.E. 24 ft. tunnel part 1 wake survey#491469AERADE
• Zero lift drag measurements on swept wings at transonic and supersonic speeds using the ground-launched rocket-boosted model technique#491497AERADE
• Report of the first year's flying on the development of flight testing techniques for finding and measuring natural icing conditions#491573AERADE
• Report of the second year's flying on the development of flight testing techniques for finding and measuring natural icing conditions#491574AERADE
• Report of the third year's flying on the development of flight testing techniques for finding and measuring natural icing conditions#491575AERADE
• Full scale measurement of impact loads on a large flying boat (sunderland MK. 5) part 3 data for impacts on main step#491692AERADE
• Direct stress fatigue tests on redux-bonded and riveted double strap joints in 10 S.W.G. aluminium alloy sheet#491705AERADE
• Experimental investigation of the pressure distribution at the centre-section of a sweptback wing at high subsonic speeds#491719AERADE
• Validation of Steering Law for a 4-Variable-Speed Single-Gimbal Control Moment Gyroscope Pyramid Cluster via Spherical Air-Bearing Testbed#651533DigitalCommons@USU
• Toward Risk-Informed Design of Supercooling Heat Exchangers: Statistical Inference and Experimental Investigation of Heterogeneous Ice Nucleation#291204DigitalCommons@USU
• Gas density structure of supersonic flows impinged on by thin blades for laser–plasma accelerator targets#619978eScholarship
• A data-based certification platform for additively manufactured metal aircraft components: considering compliance with European law and potential business cases#147705Springer Nature OA
• The indication of boundary-layer transition on aerofoils in the N.P.L. 20 in. x 8 in. high speed wind tunnel#491362AERADE
• Low-speed wind tunnel investigation of the change in aerodynamic centre position and in Cmo due to propeller turbine nacelles#491391AERADE
• Observations of the interaction between the shock waves and boundary layers at the trailing edges of aerofoils in supersonic flow#491405AERADE
• A method for calculating pressure distributions on circular arc ogives at zero incidence at supersonic speeds, using the Prandtl-Meyer flow relations#491466AERADE
• Note on an application of the tilting plate method of Mach number variation for wind tunnel tests at low supersonic speeds#491520AERADE
• Note on the flow near the tail of a two-dimensional aerofoil moving at a free-stream mach number close to unity#491540AERADE
• Full scale measurements of impact loads on a large flying boat (sunderland Mk.5) part 2 results for impacts on main step#491557AERADE
• The influence of pressure ratio and divergence angle on the shock position in two dimensional, over-expanded, convergent-divergent nozzles#491679AERADE
• Some notes on shock-wave boundary-layer interactions, and on the effect of suction on the separation of laminar boundary layers#491684AERADE
• Full scale measurements of impact loads on a large flying boat (Sunderland MK.5) part 5 results of rough water tests#491694AERADE
• Advancing Radiation Shielding in Long-Term Space Missions and Deep Space Habitats Using In-Situ Resources and Additive Manufacturing#208579Figshare
• Program and Proceedings: Nebraska Academy of Sciences 1880–2025, 145th Anniversary Year, One Hundred-Thirty-Fifth Annual Meeting#475496DigitalCommons@University of Nebraska
• CELiS: Compact Eyesafe Lidar System, A Portable 1.5 μm Elastic Lidar System for Rapid Aerosol Concentration Measurement: Part 2, Retrieval of Particulate Matter Concentration#623790DigitalCommons@USU
• AI-enabled crater-based navigation for lunar mapping#225383Springer Nature OA
• Artificial intelligence-driven design and deployment of autonomous eVTOL drones for urban air mobility: a comprehensive review of challenges, technologies, and integration strategies#316793Springer Nature OA
• Development and Verification of an Updated Thermal Model for Cal Poly's Small Thermal Vacuum Chamber#322174DigitalCommons@CalPoly
• Tests in the N.P.L. electric tank on a 4:1 axi-symmetrical diffuser having a discontinuity in the wall velocity#491354AERADE
• Report on measurements of the pressure distribution over a wing of triangular plan form at a Mach number of 2.44#491359AERADE
• A brief survey of some methods and information concerning the aerodynamic derivatives of wings in unsteady motion at transonic and supersonic speeds#491437AERADE
• Tests in the compressed air tunnel on two aerofoil sections having a large scale effect on CLmax at a critical reynolds number#491444AERADE
• Note on the effect of thickness and aspect ratio on the damping of pitching oscillations of rectangular wings moving at supersonic speeds#491503AERADE
• Calibration of the R.A.E. No. 18 (9" x 9") Supersonic Wind Tunnel. Part II:- Tests at Atmospheric Stagnation Pressure#491515AERADE
• Some visual observations of the flow over a swept-back wing in a water tunnel, with particular reference to high incidences#491544AERADE
• Some Tests on the Spread of Velocity in a Cold Jet Discharging with Excess Pressure from a Sonic Exit into Still Air#491598AERADE
• The numerical integration of the laminar compressible boundary layer equations, with special reference to the position of separation when the wall is cooled#491664AERADE
• Computational Fluid Dynamics Analysis of Moisture Ingress in Aircraft Structural Composite Materials#666647OpenAlex
• Modeling and control for heave dynamics of a flexible wing micro aerial vehicle distributed parameter system#957938Louisiana Tech Digital Commons