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Notes And Tables For Use In The Analysis Of Supersonic Flow
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Book Synopsis Notes and Tables for Use in the Analysis of Supersonic Flow by :
Download or read book Notes and Tables for Use in the Analysis of Supersonic Flow written by and published by . This book was released on 1947 with total page 594 pages. Available in PDF, EPUB and Kindle. Book excerpt: This document is a compilation of formulas, tables, and curves for use in the analysis of supersonic flow.
Book Synopsis Charts and Approximate Formulas for the Estimation of Aeroelastic Effects on the Lateral Control of Swept and Unswept Wings by : Almer D. Crim
Download or read book Charts and Approximate Formulas for the Estimation of Aeroelastic Effects on the Lateral Control of Swept and Unswept Wings written by Almer D. Crim and published by . This book was released on 1952 with total page 344 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Note written by and published by . This book was released on 1947 with total page 546 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Technical Note - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics
Download or read book Technical Note - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1958 with total page 1274 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Index of Tables and Charts for Use in Gas Dynamic Studies by : D. E. Randall
Download or read book An Index of Tables and Charts for Use in Gas Dynamic Studies written by D. E. Randall and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents a list of references which provide tabulated or graphical information regarding the atmosphere, gas flows, flow through shock waves, and information on the thermodynamic and transport properties of gases.
Book Synopsis Report by : United States. National Advisory Committee for Aeronautics
Download or read book Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1955 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Index of NACA Technical Publications by : United States. National Advisory Committee for Aeronautics
Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1949 with total page 616 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book SCR. written by and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Report - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics
Download or read book Report - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1950 with total page 996 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Tables of Characteristic Functions for Solving Boundary-value Problems of the Wave Equation with Application to Supersonic Interference by : Jack Norman Nielsen
Download or read book Tables of Characteristic Functions for Solving Boundary-value Problems of the Wave Equation with Application to Supersonic Interference written by Jack Norman Nielsen and published by . This book was released on 1957 with total page 682 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tables are presented containing 69,000 values of a set of characteristic functions which first arose in problems of supersonic wing-body interference. The tables are useful in problems of supersonic flow involving aerodynamic shapes which are wholly or in part quasi-cylinders of nearly circular cross section. A number of uses are described in the aerodynamics of bodies alone, body-body or shock-body interference, wing-body interference, the vortex-panel interference. Three illustrative examples are worked out in detail. First, the pressure field due to fuselage indentation is calculated and presented in a form independent of Mach number. Secondly, the tables are applied to a problem involving a previously unpublished solution to the Navier-Stokes equations; namely, the boundary-layer profiles of a circular cylinder moved impulsively with a constant axial force in a viscous incompressible fluid. In the final example, the wave drag of corrugated circular cylinders is calculated as a function of the number of corrugations and their wave length. Several nonaerodynamic applications are pointed out in the fields of acoustics and heat conduction. Generally speaking, the tables are applicable to boundary-value problems of the second kind involving the wave equation in three dimensions with approximately circular cylindrical boundaries or involving the unsteady heat-conduction equation in two space dimensions with nearly circular boundaries.
Book Synopsis Tables of Supersonic Flow Around Cones of Large Yaw by the Staff of the Computing Section Center of Analysis Under the Direction of Zdeněk Kopal by :
Download or read book Tables of Supersonic Flow Around Cones of Large Yaw by the Staff of the Computing Section Center of Analysis Under the Direction of Zdeněk Kopal written by and published by . This book was released on 1949 with total page 125 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Method for Determining Optimum Division of Power Between Jet and Propeller for Maximum Thrust Power of a Turbine-propeller Engine by : Arthur M. Trout
Download or read book Method for Determining Optimum Division of Power Between Jet and Propeller for Maximum Thrust Power of a Turbine-propeller Engine written by Arthur M. Trout and published by . This book was released on 1950 with total page 608 pages. Available in PDF, EPUB and Kindle. Book excerpt: Charts are presented by means of which the jet pressure ratio that give optimum division of power between propeller and jet for maximum total thrust power may be determined for any turbine-propeller engine with or without intercooling, reheat, regeneration, or any combination of these modifications.
Download or read book NASA Technical Note written by and published by . This book was released on 1970 with total page 444 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Annual Report of the National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics
Download or read book Annual Report of the National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1950 with total page 988 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Book Synopsis Mathematical Tables and Other Aids to Computation by :
Download or read book Mathematical Tables and Other Aids to Computation written by and published by . This book was released on 1948 with total page 964 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Analysis of Supersonic Flow in the Region of the Leading Edge of Curved Airfoils, Including Charts for Determining Surface-pressure Gradient and Shock-wave Curvature by : Samuel Kraus
Download or read book An Analysis of Supersonic Flow in the Region of the Leading Edge of Curved Airfoils, Including Charts for Determining Surface-pressure Gradient and Shock-wave Curvature written by Samuel Kraus and published by . This book was released on 1952 with total page 45 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flow in the region of the leading edge of curved airfoils with attached shock waves is investigated. Tables and charts are presented for determining the surface-pressure gradient and shock-wave curvature in supersonic flow of an ideal diatomic gas. The results cover a range of Mach numbers from 1.5 to infinite and deflection angles from zero up to those approaching shock detachment. Calculations of surface-pressure gradient and shock-wave curvature are also made for curved airfoils in supersonic flow of a calorically imperfect, diatomic gas. An approximate procedure for determining the flow field a short distance downstream of the leading edge is also presented.
Download or read book Technical Information Pilot written by and published by . This book was released on 1951 with total page 500 pages. Available in PDF, EPUB and Kindle. Book excerpt:
