1-17 of 17 Books

Aircraft accident report
By United States. National Transportation Safety Board.
Low-speed wind-tunnel parametric investigation of flight spoilers as trailing-vortex-alleviation devices on a transport aircraft model
Low-speed wind-tunnel parametric investigation of flight spoilers as trailing-vortex-alleviation devices on a transport aircraft model
By Delwin R. Croom
Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control
Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control
By A. B. Blair
Low-speed aerodynamic characteristics of a highly swept, untwisted, uncambered arrow wing
Low-speed aerodynamic characteristics of a highly swept, untwisted, uncambered arrow wing
By Paul L. Coe
737 graphite composite flight spoiler flight service evaluation
737 graphite composite flight spoiler flight service evaluation
By Randy L. Coggeshall
Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control
Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control
By A. B Blair
Low-speed wind-tunnel parametric investigation of flight spoilers as trailing-vortex-alleviation devices on a transport aircraft model
Low-speed wind-tunnel parametric investigation of flight spoilers as trailing-vortex-alleviation devices on a transport aircraft model
By Delwin R Croom
Low-speed aerodynamic characteristics of a highly swept, untwisted, uncambered arrow wing
Low-speed aerodynamic characteristics of a highly swept, untwisted, uncambered arrow wing
By Paul L Coe
A developed theory of spoilers on aerofoils
A developed theory of spoilers on aerofoils
By C. S. Barnes
Two-dimensional normal fences on a flat plate
Two-dimensional normal fences on a flat plate
By C. S. Barnes
Ground spoiler activation in flight/hard landing, ValuJet Airlines flight 558, Douglas DC-9-32, N922VV, Nashville, Tennessee, January 7, 1996
Ground spoiler activation in flight/hard landing, ValuJet Airlines flight 558, Douglas DC-9-32, N922VV, Nashville, Tennessee, January 7, 1996
By United States. National Transportation Safety Board.
Untersuchungen von Strahlspoilern im Überschall im Hinblick auf eine Anwendung für die Kraftstoffspritzung
Untersuchungen von Strahlspoilern im Überschall im Hinblick auf eine Anwendung für die Kraftstoffspritzung
By U. Ganzer

Flow field measuremnts of an airfoil with deflected spoiler using a two-component LDV sys
By Michael J. Foreman
Aerodynamic spoiler for preventing airplane stall/spin type accidents
Aerodynamic spoiler for preventing airplane stall/spin type accidents
By H. I. Chevalier
Flight evaluation of a spoiler roll control system on a light twin-engine airplane
Flight evaluation of a spoiler roll control system on a light twin-engine airplane
By David L. Kohlman
Simulator evaluation of a flight-path-angle control system for a transport airplane with direct lift control
Simulator evaluation of a flight-path-angle control system for a transport airplane with direct lift control
By Wendell W Kelley
Feasibility study of aileron and spoiler control systems for large horizontal axis wind turbines
Feasibility study of aileron and spoiler control systems for large horizontal axis wind turbines
By