The Wing-body Interference Problem for Linearized Supersonic Flow PDF Download

Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download The Wing-body Interference Problem for Linearized Supersonic Flow PDF full book. Access full book title The Wing-body Interference Problem for Linearized Supersonic Flow by Michael Chen-Chiang Fong. Download full books in PDF and EPUB format.

The Wing-body Interference Problem for Linearized Supersonic Flow

The Wing-body Interference Problem for Linearized Supersonic Flow PDF Author: Michael Chen-Chiang Fong
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 68

Book Description


The Wing-body Interference Problem for Linearized Supersonic Flow

The Wing-body Interference Problem for Linearized Supersonic Flow PDF Author: Michael Chen-Chiang Fong
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 68

Book Description


The Wing-body Problem for Linearized Supersonic Flow

The Wing-body Problem for Linearized Supersonic Flow PDF Author: George K. Morikawa
Publisher:
ISBN:
Category : Electronic dissertations
Languages : en
Pages : 138

Book Description


On the Determination of Certain Basic Types of Supersonic Flow Fields

On the Determination of Certain Basic Types of Supersonic Flow Fields PDF Author: Carlo Ferrari
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 26

Book Description
Abstract: A discussion is given of the application of Fourier series techniques to the problems of linearized supersonic flow. The formulation presented is an extension of the doublet type of "fundamental solution" to higher order types of singularity. The equations developed have application to wing theory but are primarily of importance in wing-body interaction problems. A specific example of a wing-body interference problem is discussed in light of the presented methods.

An Integrated Approach to the Analysis and Design of Wings and Wing-body Combinations in Supersonic Flow

An Integrated Approach to the Analysis and Design of Wings and Wing-body Combinations in Supersonic Flow PDF Author: Ralph L. Carmichael
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 18

Book Description


Reverse Flow and Supersonic Interference

Reverse Flow and Supersonic Interference PDF Author: Brown University. Division of Engineering
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 106

Book Description


On Wing-body Interference in Supersonic Flow

On Wing-body Interference in Supersonic Flow PDF Author: K. Stewartson
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

Book Description


Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 994

Book Description


An Analysis of the Stability and Ultimate Compressive Strength of Short Sheet-stringer Panels with Special Reference to the Influence of the Riveted Connection Between Sheet and Stringer

An Analysis of the Stability and Ultimate Compressive Strength of Short Sheet-stringer Panels with Special Reference to the Influence of the Riveted Connection Between Sheet and Stringer PDF Author: Benjamin H. Beam
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 312

Book Description


Progress Report No. 4, Wing-Body Interference

Progress Report No. 4, Wing-Body Interference PDF Author: R. E. Phinney
Publisher:
ISBN:
Category :
Languages : en
Pages : 46

Book Description


Tables of Characteristic Functions for Solving Boundary-value Problems of the Wave Equation with Application to Supersonic Interference

Tables of Characteristic Functions for Solving Boundary-value Problems of the Wave Equation with Application to Supersonic Interference PDF Author: Jack Norman Nielsen
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 682

Book Description
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.