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ransonic-aerodynamic-characteristics-of-wings-having</loc><lastmod>2026-09-21T15:06:14.667Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086756/altitude-wind-tunnel-investigation-of-performance-characteristics-of-a-j47d-prototype-rx1-1-turbojet</loc><lastmod>2026-09-21T15:06:14.669Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086758/experimental-investigation-of-effect-of-jet-exit-configuration-on-thrust-and-drag</loc><lastmod>2026-09-21T15:06:14.669Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086767/estimation-of-neutron-energy-for-first-resonance-from-absorption-cross-section-for-thermal-neutrons</loc><lastmod>2026-09-21T15:06:14.670Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086786/investigation-at-mach-number-1-88-of-half-of-a-conical-spike-diffuser-mounted-as-a-side-inlet-with-b</loc><lastmod>2026-09-21T15:06:14.671Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086787/damping-in-roll-of-rocket-powered-test-vehicles-having-swept-tapered-wings-of-low-aspect-ratio</loc><lastmod>2026-09-21T15:06:14.674Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086803/investigation-of-a-24-inch-shock-in-rotor-type-supersonic-compressor-designed-for-simple-radial-equi</loc><lastmod>2026-09-21T15:06:14.675Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086811/stability-and-control-measurements-obtained-during-usaf-naca-cooperative-flight-test-program-on-the</loc><lastmod>2026-09-21T15:06:14.680Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086813/flame-velocities-over-a-wide-composition-range-for-pentane-air-ethylene-air-and-propyne-air-flames</loc><lastmod>2026-09-21T15:06:14.681Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086815/determination-and-use-of-the-local-recovery-factor-for-calculating-the-effectiveness-gas-temperature</loc><lastmod>2026-09-21T15:06:14.683Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086825/preliminary-investigation-of-a-supersonic-scoop-inlet-derived-from-a-conical-spike-nose-inlet</loc><lastmod>2026-09-21T15:06:14.684Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086826/wind-tunnel-investigation-of-the-aerodynamic-characteristics-of-a-1-15-scale-model-of-the-northrop-m</loc><lastmod>2026-09-21T15:06:14.684Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086830/studies-of-the-use-of-freon-12-as-a-testing-medium-in-the-langley-low-turbulence-pressure-tunnel</loc><lastmod>2026-09-21T15:06:14.685Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086833/comparison-of-naca-65-series-compressor-blade-pressure-distributions-and-performance-in-a-rotor-and</loc><lastmod>2026-09-21T15:06:14.685Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086836/tests-in-the-ames-40-by-80-foot-wind-tunnel-of-an-airplane-configuration-with-an-aspect-ratio-4-tria</loc><lastmod>2026-09-21T15:06:14.686Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086840/a-flight-evaluation-of-the-longitudinal-stability-characteristics-associated-with-the-pitch-up-of-a</loc><lastmod>2026-09-21T15:06:14.686Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086844/analytical-investigation-of-two-liquid-cooling-systems-for-turbine-blades</loc><lastmod>2026-09-21T15:06:14.687Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086853/preliminary-evaluation-of-the-air-and-fuel-specific-impulse-characteristics-of-several-potential-ram</loc><lastmod>2026-09-21T15:06:14.688Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086858/flight-investigation-at-subsonic-transonic-and-supersonic-velocities-of-the-hinge-moment-characteris</loc><lastmod>2026-09-21T15:06:14.689Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086863/performance-of-single-stage-compressor-designed-on-basis-of-constant-total-enthalpy-with-symmetrical</loc><lastmod>2026-09-21T15:06:14.690Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086879/preliminary-investigation-of-a-translating-cowl-technique-for-improving-take-off-performance-of-a-sh</loc><lastmod>2026-09-21T15:06:14.691Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086886/comparison-of-semispan-and-full-span-tests-of-a-47-5-degrees-sweptback-wing-with-symmetrical-circula</loc><lastmod>2026-09-21T15:06:14.693Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086894/investigation-of-the-effect-of-a-nacelle-at-various-chordwise-and-vertical-positions-on-the-aerodyna</loc><lastmod>2026-09-21T15:06:14.693Z</lastmod></url><url><loc>https://engineeringpapers.com/record/nasa%3A19930086957/preliminary-investigation-of-the-t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