A method of characteristics for steady three- dimensional supersonic flow with application to inclined bodies of revolution
Characteristics method for determining three dimensional supersonic flow around inclined body of revolution
Rakich, J. V.↗
SEARCH · Engineering Papers
Results for “REVOLUTION”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Nonlinear analysis of shells of revolution by the matrix displacement method.
Matrix displacement method for nonlinear elastic analysis of shells of revolution under symmetrical and asymmetrical loadings
Haisler, W. E.↗
Aerodynamics of bodies of revolution in coning motion.
Aerodynamics of bodies of revolution in nonplanar motion using nonlinear functional analysis of moments for motion about center of gravity
Peterson, V. L.↗
Post-wrinkling behavior of a conical shell of revolution subjected to bending loads.
Post-wrinkling nonlinear behavior of conical shell of revolution subjected to bending loads
Conroy, D. C.↗
A geometrically exact finite element for thin shells of revolution.
Geometrically exact finite element for thin shells of revolution, using approximation to predict boundary layer stress distribution during vibration
Adelman, H. M.↗
Determination of Shapes of Boattail Bodies of Revolution for Minimum Wave Drag
By use of an approximate equation for the wave drag of slender bodies of revolution in a supersonic flow field, the optimum shapes of certain boattail bodies are determined for minimum wave drag. The properties of three specific families of bodies are determined, the first family consisting of bodies having a given length and base area and a contour passing through a prescribed point between the nose and base, the second family having fixed length, base area, and maximum area, and the third family having given length, volume, and base area. The method presented is easily generalized to determine minimum-wave-drag profile shapes which have contours that must pass through any prescribed number of points. According to linearized theory, the optimum profiles are found to have infinite slope at the nose but zero radius of curvature so that the bodies appear to have pointed noses, a zero slope at the body base, and no variation of wave drag with Mach number. For those bodies having a specified intermediate.diameter (that is, location and magnitude given), the maximum body diameter is shown to be larger, in general, than the specified diameter. It is also shown that, for bodies having a specified maximum diameter, the location of the maximum diameter is not arbitrary but is determined from the ratio of base diameter to maximum diameter.
Adams, Mac C.↗
Numerical analysis of shells. Volume 1 - Unsymmetric analysis of orthotropic reinforced shells of revolution
Analysis of thin orthotropic shells of revolution subjected to unsymmetric loading - Vol. 1
Svalbonas, V.↗
Theoretical investigation of crossflow effects on compressible turbulent boundary layer over bodies of revolution
Crossflow effects on compressible turbulent boundary layer over bodies of revolution
Calarese, W.↗
Procedures for designing supersonic bodies of revolution from prescribed surface pressure distributions
Iterative method for designing supersonic body of revolution from surface pressure distribution
Barger, R. L.↗
Generalized ring stiffness matrix for ring- stiffened shells of revolution
Generalized ring stiffness matrix for ring stiffened shells of revolution
Walz, J. E.↗
Prediction of the position and velocity of a satellite after many revolutions
Position and velocity prediction method for satellite after many revolutions
Dallas, S. S.↗
Nonlinear dynamic analysis of shells of revolution by matrix displacement method
Nonlinear dynamic analysis of shells of revolution by matrix displacement method
Haisler, W. E.↗
Analysis of shells of revolution having arbitrary stiffness distributions
Shells of revolution having arbitrary stiffness distribution and subjected to arbitrary loads and temperatures
Cappelli, A. P.↗
Linear and nonlinear static analysis of axisymmetrically loaded thin shells of revolution
Finite element method analysis of axisymmetrically loaded thin shells of revolution, considering nonlinearity due to material properties and shell geometry changes
Popov, E. P.↗
Nonlinear aerodynamics of bodies of revolution in free flight
Nonlinear aerodynamic moments for arbitrary motions of bodies of revolution in free flight
Levy, L. L., Jr.↗
On the calculation of static and dynamic stability derivatives for bodies of revolution at subsonic and transonic speeds
Stability derivatives for bodies of revolution at subsonic and transonic speeds
Liu, D. D.↗
Natural vibrations of laminated orthotropic shells of revolution
Natural vibration frequencies and mode shapes for laminated orthotropic shells of revolution using finite element method
Dong, S. B.↗
Computer analysis of imperfection sensitivity of ring-stiffened orthotropic shells of revolution
Stability analysis of ring-stiffened orthotropic, multilayered shells of revolution under axisymmetric torsionless loads by digital computer
Cohen, G. A.↗