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Low-speed wind-tunnel investigation of lateral control characteristics of a 60 degrees triangular-wing model having half-delta tip controls
Report presenting a low-speed investigation in the stability tunnel to determine the lateral control characteristics of a 60 degree triangular wing model equipped with half-delta tip controls with areas of 5, 10, and 15 percent of the wing area. Results regarding lateral control effectiveness, rolling effectiveness, and a comparison of control and effectiveness with theory are provided.
Date:
November 27, 1951
Creator:
Jaquet, Byron M. & Queijo, M. J.
System:
The UNT Digital Library
Load distribution over a fuselage in combination with a swept wing at small angles of attack and transonic speeds
Report presenting free-fall tests of a wing-body configuration with a 45 degree sweptback cambered and twisted wing of aspect ratio 6 on a fuselage of fineness ratio 12.4. Results regarding the load and pitching moments and load-coefficient distribution are provided.
Date:
November 27, 1951
Creator:
White, Maurice D. & Look, Bonne C.
System:
The UNT Digital Library