Byron M Jaquet

发表

Effect of fuselage and tail surfaces on low-speed yawing characteristics of a swept-wing model as determined in curved-flow test section of Langley stability tunnel

John D Bird, Byron M Jaquet, John W Cowan, 1951 .

Low-speed pitching derivatives of low-aspect-ratio wings of triangular and modified triangular plan forms

Byron M Jaquet, Alex Goodman, 1950 .

Effects of chord discontinuities and chordwise fences on low-speed static longitudinal stability of an airplane model having a 35 degree sweptback wing

Byron M Jaquet, B. M. Jaquet, 1952 .

A study of the use of experimental stability derivatives in the calculation of the lateral disturbed motions of a swept-wing airplane and comparison with flight results

John D Bird, Byron M Jaquet, 1951 .

Effects of Horizontal-tail Position and Aspect Ratio on Low-speed Static Longitudinal Stability and Control Characteristics of a 60 Degree Triangular-wing Model Having Twin Triangular All-movable Tails

Byron M Jaquet, 1952 .

Effects of chord-extension and droop of combined leading edge flap and chord-extension on low-speed static longitudinal stability characteristics of an airplane model having a 35 degree sweptback wing with plain flaps neutral or deflected

Byron M Jaquet, 1953 .

Effects of Horizontal-tail Position, Area, and Aspect Ratio on Low-speed Static Longitudinal Stability and Control Characteristics of a 60 Degrees Triangular-wing Model Having Various Triangular-all-movable Horizontal Tails

Byron M Jaquet, 1951 .

Wind-Tunnel Investigation at Low Speed of the Effects of Chordwise Wing Fences and Horizontal-Tail Position on the Static Longitudinal Stability Characteristics of an Airplane Model with a 35 Degree Sweptback Wing

Byron M Jaquet, Walter D Wolhart, M J Queijo, 1954 .