1-24 of 40 Books
Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment
Navier-Stokes and potential theory solutions for a helicopter fuselage and comparison with experiment
By Mark S. Chaffin
Vibro-acoustics modal testing at NASA Langley Research Center
Vibro-acoustics modal testing at NASA Langley Research Center
By Richard S. Pappa
Water-tunnel study results of a TF/A-18 and F/A-18 canopy flow visualization
Water-tunnel study results of a TF/A-18 and F/A-18 canopy flow visualization
By Steven A. Johnson
Two-dimensional aerodynamic characteristics of several polygon-shaped cross-sectional models applicable to helicopter fuselages
Two-dimensional aerodynamic characteristics of several polygon-shaped cross-sectional models applicable to helicopter fuselages
By Henry L. Kelley
Crashworthy evaluation of a 1/5-scale model composite fuselage concept
Crashworthy evaluation of a 1/5-scale model composite fuselage concept
By Karen E. Jackson
Computation of three-dimensional compressible boundary-layers to fourth-order accuracy on wings and fuselages
Computation of three-dimensional compressible boundary-layers to fourth-order accuracy on wings and fuselages
By Venkit Iyer
Rotor-fuselage interactions
Rotor-fuselage interactions
By Barry, John D.
Compression response of a sandwich fuselage keel panel with and without damage
Compression response of a sandwich fuselage keel panel with and without damage
By David M. McGowan
Evaluation of pressurization fatigue life of 1441 Al-Li fuselage panel
Evaluation of pressurization fatigue life of 1441 Al-Li fuselage panel
By R. Keith Bird
Numerical simulation of helicopter engine plume in forward flight
Numerical simulation of helicopter engine plume in forward flight
By Arsenio C. B. Dimanlig
Analytical studies of boundary layer generated aircraft interior noise
Analytical studies of boundary layer generated aircraft interior noise
By M. S. Howe
Experimental measurement of structural power flow on an aircraft fuselage
Experimental measurement of structural power flow on an aircraft fuselage
By J. M. Cuschieri
NASA airframe structural integrity program
NASA airframe structural integrity program
By Charles E. Harris
A review of ice accretion data from a model rotor icing test and comparison with theory
A review of ice accretion data from a model rotor icing test and comparison with theory
By Randall K. Britton
Design of fuselage shapes for natural laminar flow
Design of fuselage shapes for natural laminar flow
By Simha S. Dodbele
Analysis and design of fuselage structures including residual strength prediction methodology
Analysis and design of fuselage structures including residual strength prediction methodology
By Norman F. Knight
A record of all marker bands found in the upper rivet rows of 2 adjacent bays from a fuselage lap splice joint
A record of all marker bands found in the upper rivet rows of 2 adjacent bays from a fuselage lap splice joint
By Scott A. Willard
Influence of an asymmetric ring on the modeling of an orthogonally stiffened cylindrical shell
Influence of an asymmetric ring on the modeling of an orthogonally stiffened cylindrical shell
By Naveen Rastogi
Design and fabrication of a sealed composite fuselage section for the UTIAS Crash Program
Design and fabrication of a sealed composite fuselage section for the UTIAS Crash Program
By James Robert Bruce Johnston
The effects of fuselage flexibility on ultralight aircraft design
The effects of fuselage flexibility on ultralight aircraft design
By Marco Papini
Fuselage design for a specified Mach-sliced area distribution
Fuselage design for a specified Mach-sliced area distribution
By Raymond L. Barger
A study of crashworthiness of light aircraft fuselage structures
A study of crashworthiness of light aircraft fuselage structures
By Asifa Peter Nanyaro
Novel composites for wing and fuselage applications
Novel composites for wing and fuselage applications
By Larry H. Sobel
Development of stitched/RTM primary structures for transport aircraft
Development of stitched/RTM primary structures for transport aircraft
By Arthur V. Hawley