NEWS OF INSTITUTIONS OF HIGHER LEARNING. AERONAUTICAL ENGINEERING (COLLECTION OF ARTICLES)
Abstract
Contents: Analysis of weight characteristics of fuel tanks of flight vehicles with liquid-propellant engines; Solution of problems of bending of three-layered plates and shells by means of a displacement function; Calculation of the nonaxially symmetric state of strain of cylindrical shells taking into account the elasticity of the reinforcing frames; Vibrations of an anisotropic plate under a continuously moving distributed load; Edge effect during the joint action of axial and radial pressure for anisotropic circular cylindrical shells; Application of the method of asymptotic integration to problems of vibrations of shells of revolution which are similar in form to spherical shells; Calculation of closed cylindrical and slightly conical shells with arbitrary contour of cross section; Experimental investigation of the propagation of fan and paired plane jets in a transverse flow; Method of supersonic analogy for calculation of one-dimensional non-stationary gas flows; Optimum compression in the compressor of a ducted-fan turbojet engine with an afterburner; Approximate method of estimating gas-dynamic influence on a supersonic flow; Influence of a sequential decrease in thickness of a metal on the curvature of shaped components; Approximate calculation of speed of flight in a slanted dive and determination of loss in altitude and range on the dive entry section on a program for a pilotless aircraft with turbojet engine.
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1965
- Accession Number
- AD0628788