Acoustic transmission through a fuselage sidewall [PDF]
A definition is given of an idealized fuselage sidewall structure and a simplified analytical model for determining acoustical transmission from the exterior to the interior of a fuselage was constructed.
Scharton, T. D., Wilby, J. F.
core +1 more source
Oblique-wing supersonic aircraft [PDF]
, 1976 An aircraft including a single fuselage having a main wing and a horizontal stabilizer airfoil pivotally attached at their centers to the fuselage is described.
Jones, R. T.
core +1 more source
Preliminary wind-tunnel investigation of the effects of engine nacelles on a transport configuration with high lift drag ratios to a Mach number of 1.00 [PDF]
Wind tunnel tests to determine the effect of engine nacelles added to a low wing fuselage vertical tail configuration utilizing the NASA supercritical airfoil and a refined area ruled fuselage are discussed.
Flechner, S. G.
core +1 more source
TO THE DEVELOPMENT OF AERODYNAMIC SHAPE OF MEDIUM SIZED PERSPECTIVE HELICOPTER FUSELAGE
Научный вестник МГТУ ГА, 2017 This paper presents the initial stage of work out of the helicopter body aerodynamic configuration. The main purpose of this work is to design the model of the fuselage and to minimize its drag.The analysis of experimental data obtained in TsAGI and ...
V. A. Vershkov +2 more
doaj
RESEARCH ON TEST METHOD OF FUSELAGE PANEL SUBJECTED TO SHEAR LOAD
Jixie qiangdu, 2017 The test method of fuselage panel subjected to shear load is an important technique for aircraft structure strength research. A new shear test method is proposed based on the property of aircraft fuselage panel subjected to shear load.
ZANG WeiFeng +3 more
doaj
Aerodynamic characteristics of an NASA supercritical-wing research airplane model with and without fuselage area-rule additions at Mach 0.25 to 1.00 [PDF]
Transonic pressure tunnel tests at Mach numbers from 0.25 to 1.00 were performed to determine the effects of area-rule additions to the sides of the fuselage on the aerodynamic characteristics of a 0.087 scale model of an NASA supercritical-wing research
Bartlett, D. W., Harris, C. D.
core +1 more source
, 1975 A space vehicle having an improved ascent configuration for use in traveling in space is presented. Components of the vehicle are: (1) a winged orbiter having an elongater fuselage and rearwardly directed main engines fixed to the fuselage; (2) an ...
Vonpragenau, G. L.
core +1 more source
Fabrication of the V-22 composite AFT fuselage using automated fiber placement [PDF]
Boeing Helicopters and its subcontractors are working together under an Air Force Wright Research and Development Center (WRDC)-Manufacturing-Technology Large-Composite Primary Structure Fuselage program to develop and demonstrate new manufacturing ...
Pinckney, Robert L.
core +1 more source
Unified aeroacoustics analysis for high speed turboprop aerodynamics and noise. Volume 5: Propagation of propeller tone noise through a fuselage boundary layer [PDF]
An analysis of tone noise propagation through a boundary layer and fuselage scattering effects was derived. This analysis is a three dimensional and the complete wave field is solved by matching analytical expressions for the incident and scattered waves
Hanson, D. B., Magliozzi, B.
core +1 more source
Instantaneous baseline damage localisation using sensor mapping [PDF]
, 2016 In this paper an instantaneously recorded baseline method is proposed using piezoelectric transducers for damage localisation under varying temperature.
Aliabadi, MH +2 more
core +1 more source