aerospace-engineering

Documents about aerospace-engineering

• Tables of aerodynamic flutter derivatives for thin wings and control surfaces in two dimensional supersonic flow#491734AERADE
• Reacquiring Satellites After Unknown Maneuvers in Sensor Blind Spots: A Physics-Informed Behavioral Framework for Closed-Loop Custody Recovery#651525DigitalCommons@USU
• Data-Driven LPV Modeling via Parametric DMD and Predictive Control of Highly Flexible Aircraft#325545DigitalCommons@USU
• Distributed Coherent Beamforming at 60 GHz Enabled by Optically-Established Coherence#623781DigitalCommons@USU
• Potential Airborne Optical Contributions to the European Phased Adaptive Approach (EPAA) for Missile Defense#623785DigitalCommons@USU
• Impact of Finite Swept Wings on Leading-Edge Vortex Structure and Stability under Impulsive Conditions#634757eScholarship
• A2S Uplink Latency Minimization for Wildfire Monitoring Systems Using MBSE and Stochastic Modeling#398456DigitalCommons@CalPoly
• Transient behavior of a supersonic three-dimensional micronozzle with an intersecting capillary#611932eScholarship
• Additive manufacturing (3D printing): A review of materials, methods, applications and challenges#7123OpenAlex
• Efficient multigrid algorithms for higher order Discontinuous Galerkin discretizations of turbulent flows#217587electronic library
• Aircraft Structural Dynamics and Aeroelasticity Approaches: Recent Contributions from the Aerospace Engineering of Middle East Technical University, Türkiye#483496OpenMETU
• Tank tests on the effect of slipstream on the water performance of a large four engined flying boat (Shetland 1)#491358AERADE
• Wind tunnel tests on a one-twelfth scale model of a twin-engined military transport. (airspeed C 13/45 ayrshire)#491369AERADE
• Wind tunnel tests on the effect of accretion of ice on control characteristics in two-dimensional flow#491394AERADE
• Free flight measurements at supersonic speeds of the drag of a particular delta wing having a simple pressure distribution#491409AERADE
• Pressure measurements in a supersonic tunnel on a two-dimensional aerofoil of R.A.E. 104 section#491414AERADE
• An approximate method of deriving the transient response of a linear system from the frequency response#491465AERADE
• Criteria for condensation free flow in the R.A.E. no. 18 (9" x 9") supersonic tunnel#491516AERADE
• Full scale measurements of impact loads on a large flying boat part 1 description of apparatus and instrument installation#491534AERADE
• Approximate wall corrections for an oscillating swept wing in a wind tunnel of closed circular section#491536AERADE
• Calibration of the flow in the working section of the 3 ft x 3 ft tunnel, National Aeronautical Establishment#491613AERADE
• Some advantages and disadvantages of variable and non-linear gearing between the pilot's control and the control surface#491615AERADE
• The influence of design pressure ratio and divergence angle on the thrust of convergent-divergent propelling nozzles#491677AERADE
• The operation of the N.P.L. 18 inches x 14 inches wind tunnel in the transonic speed range#491690AERADE
• The geometry of wing surfaces generated by straight lines and with a high rate of thickness taper at the root#491735AERADE
• Development of multi-microphone acoustic impedance tubes to measure at frequencies higher than 10 kHz#623663Digital Commons @ Michigan Tech
• Rad-Hard Circuits for Complete System-on-Chip Integration of SmallSat Electronics on Standard Non-Rad-Hard CMOS Including FinFETs#651523DigitalCommons@USU
• Active learning strategy for excursion-set confidence regions of functional simulator outputs#685158HAL (France)
• A Computational Approach to Graduated Centrifuge Profiles for Partial Gravity Planetary Environments#626216ODU Digital Commons
• Chapter 19: AeroFeathers: Biomimetic Propellers with 3D-printed Flexible Fibres for Quieter Drones#370066Digital Commons @ Michigan Tech
• A hybrid adaptive low-Mach number/compressible method: Euler equations#614718eScholarship
• Comparison of Gravity Waves Observed by Atmospheric Waves Experiment (AWE) and Simulated by High-Resolution WACCM-X#623743DigitalCommons@USU
• Higher Order Multigrid Algorithms for a 2D and 3D RANS-kw DG-Solver#217586electronic library
• Geospatial Technologies for Flood and Drought Management: A Review of Earth Observation Data, Procedures, and their Operational Effectiveness#376512Springer Nature OA
• Note on the interference on a part-wing mounted symmetrically on one wall of a wind-tunnel of octagonal section#491357AERADE
• Note on sintered metal with a view to its use as a porous surface in distributed suction experiments#491361AERADE
• The effect of propeller thrust on downwash and velocity at tailplane - a collection of data from low speed wind tunnel tests#491373AERADE
• Cockpit lighting a general survey of the principles and techniques with particular reference to the development of the dual system#491388AERADE
• Effect of mean stress on the fatigue strength of D.T.D. 364 round bars with and without transverse holes#491472AERADE
• The performance of some typical turbo-jet engine exhaust systems, with particular reference to the effects of swirl#491482AERADE
• The rapid, accurate prediction of pressure on non-lifting ogival heads of arbitrary shape, at supersonic speeds#491506AERADE
• Calibration of the R.A.E. No. 18 (9" x 9") supersonic wind tunnel part 1 preliminary investigations#491514AERADE
• Shadowgraphs of model projectiles fired at high mach numbers and near M = 1 in the N.P.L. Ballistic range#491541AERADE
• Tests on a swept-back wing and body with endplates and wing tip tanks in the compressed air tunnel#491548AERADE
• The theoretical wave drag of open-nose axisymmetrical forebodies with varying fineness ratio, area ratio and nose angle#491597AERADE
• Tests of Humidity Effects on Flow in a Wind Tunnel at Mach Numbers between 2.48 and 4#491599AERADE
• Boundary layer measurements on 10 degrees and 20 degrees cones at M = 2.45 and zero heat transfer#491616AERADE
• Low speed wind tunnel tests on perforated square flat plates normal to the airstream drag and velocity fluctuation measurements#491675AERADE
• Full scale measurements of impact loads on a large flying boat (sunderland 5) part 4 data for impacts on the afterbody#491693AERADE
• The calibration at transonic speeds of a mark 9A pitot static head with and without flow through the static slots#491736AERADE