aerospace-engineering

Documents about aerospace-engineering

• The influence of the method of stringer attachment on the buckling and failure of skin panels with square top-hat stringers an abstract from the thesis of E.E. Labram, D.C.Ae#491445AERADE
• Investigation of high length/beam ratio seaplane hulls with high beam loadings hydrodynamic stability part 14 the effect of a tailored afterbody on stability and spray characteristics with test data on model J#491703AERADE
• Investigation of high length/beam ratio seaplane hulls with high beam loadings hydrodynamic stability part 19 the interaction of the effects of forebody warp, afterbody length and afterbody angle on longitudinal stability characteristics#491704AERADE
• Raw data and data processed into graphs for the book chapter entitled: Tailoring the tribo-mechanical properties of commonly used automotive/aerospace materials#206699RepOD Dataverse OAI Archive
• The measurement of heat transfer and skin friction at supersonic speeds part 3 measurements of overall heat transfer and of the associated boundary layers on a flat plate at Ml = 2.43#491491AERADE
• Wind tunnel tests on a 90 degrees apex delta wing of variable aspect ratio (sweepback 36.8 degrees) part 1 general stability part 2 measurements of downwash and effect of high lift devices#491435AERADE
• Pressure distribution and boundary layer investigations on 44 degree swept-back tapered wing part 1 three-dimensional tests on the wing part 2 two-dimensional pressure distribution tests on 10 per cent thick symmetrical aerofoil section#491489AERADE
• Numerical Investigation on Lightning Survivability and Residual Strength of Scarf-Patched and Z-Pinned CFRP Composites#169171DigitalCommons@USU
• A Numerical Study of Acoustic Scattering of a NACA 0012 Airfoil with a Shielding Flap by the Time-Domain Boundary Element Method#412724ODU Digital Commons
• Investigation of high length/beam ratio seaplane hulls with high beam loadings hydrodynamic stability part 2 the effect of changes in the mass, moment of inertia and radius of gyration on longitudinal stability limits#491554AERADE
• SpaceOTTER: A Floating Spacecraft Simulator Air Bearing Vehicle for Hardware-In-The-Loop Experiments and Research#314561DigitalCommons@CalPoly
• TECHNICAL PROPOSAL: ÍSCARO-ALFA SWARM Hybrid Mission for Orbital Surveillance, Planetary Defense, and In-Route Dynamic Resource Harvesting (VERSION III)#210831Figshare
• Measurements of the effect of surface cooling on boundary layer transition on a 15 degrees cone part 1 tests at M = 2 and 3 in an 8 in. x 9 in. wind tunnel at R.A.E./Bedford#491733AERADE
• An experimental verification of the theoretical conclusions of R.A.E. technical note no. structures 156 (A.R.C., C.P. no. 286) "a constructional method for minimising the no. structures 156 (A.R.C., C.P. no. 286) "a constructional method for minimising th#491709AERADE
• Icarus-Defense System: Inner Heliocentric Orbit Network for Early Warning and Cosmic Threat Mitigation / Sistema Icaro-Defensa: Red de Orbita Heliocentrica Interior para Alerta Temprana y Mitigacion de Amenazas Cosmicas#191682Figshare
• Topological Flame Bifurcation, Aerodynamic Flashback Margins, and Multi-Pathway NOx Scaling in a 3D Swirl-Stabilized 100% Pure Hydrogen Aero-Engine Combustor#780702Figshare