Browse TRAIL Inventories

Characteristics of flap-type spoiler ailerons at various locations on a 60 degree delta wing with a double slotted flap

Lateral control characteristics of two structural similar flexible wings with 45 degrees sweep: a sweptback wing and a wing with M plan form

Effect of several jet-engine air-inlet configurations on the low-speed static longitudinal stability characteristics and quantity flow of a 1/6-scale model of the MX-1764 airplane

The effect of several jet-engine air-inlet configurations on the low-speed static lateral stability characteristics of a 1/6-scale model of the MX-1764 airplane

The Effect of Several Jet-Engine Air-Inlet Configurations on the Low-Speed Static Lateral Stability Characteristics of a 1/6- Scale of the MX-1764 Airplane

Effect of Several Jet-Engine Air-Inlet Configurations on the Low-Speed Static Longitudinal Stability Characteristics and Quantity Flow of a 1/6-Scale Model of the MX-1764 Airplane

A low-speed investigation of a thin 60©� delta wing equipped with a double slotted flap to determine the chordwise pressure distribution and the effect of vane size

An investigation of forward-located fixed spoilers and deflectors as gust alleviators on an unswept-wing model

Low-speed pressure-distribution investigation of a thin-delta-wing-fuselage model with double slotted flap, extended double slotted flap, and canard

Investigation of deflectors as gust alleviators on a 0.09-scale model of the Bell X-5 airplane with various wing sweep angles from 20 degrees to 60 degrees at Mach numbers from 0.40 to 0.90

Investigation at low speeds of deflectors and spoilers as gust alleviators on a model of the Bell X-5 airplane with 35 degree swept wings and on a high-aspect-ratio 35 degree swept-wing-fuselage model

Investigation at transonic speeds of deflectors and spoilers as gust alleviators on a 35 degree swept wing: transonic bump method

Low-speed pressure-distribution investigation of a thin-delta-wing-fuselage model having double slotted flaps and spoilers

Low-subsonic investigation to determine the chordwise pressure distribution and effectiveness of spoilers on a thin, low-aspect-ratio, unswept, untapered, semispan wing and on the wing with leading and trailing-edge flaps

Low-Speed Boundary-Layer-Control Investigation on a Thin Rectangular Semispan Wing With Leading-Edge and Trailing-Edge Flaps


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