Oxidation of Titanium Carbide Base Ceramals Containing Molybdenum, Tungsten, and Cobalt 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 Oxidation of Titanium Carbide Base Ceramals Containing Molybdenum, Tungsten, and Cobalt PDF full book. Access full book title Oxidation of Titanium Carbide Base Ceramals Containing Molybdenum, Tungsten, and Cobalt by M. J. Whitman. Download full books in PDF and EPUB format.

Oxidation of Titanium Carbide Base Ceramals Containing Molybdenum, Tungsten, and Cobalt

Oxidation of Titanium Carbide Base Ceramals Containing Molybdenum, Tungsten, and Cobalt PDF Author: M. J. Whitman
Publisher:
ISBN:
Category : Ceramic materials
Languages : en
Pages : 56

Book Description
The cobalt ceramals were considered better than the tungsten caramals in over-all oxidation resistance and the molybdenum ceramals were inferior to both the cobalt and tungsten ceramals.

Oxidation of Titanium Carbide Base Ceramals Containing Molybdenum, Tungsten, and Cobalt

Oxidation of Titanium Carbide Base Ceramals Containing Molybdenum, Tungsten, and Cobalt PDF Author: M. J. Whitman
Publisher:
ISBN:
Category : Ceramic materials
Languages : en
Pages : 56

Book Description
The cobalt ceramals were considered better than the tungsten caramals in over-all oxidation resistance and the molybdenum ceramals were inferior to both the cobalt and tungsten ceramals.

Rectangular-wind-tunnel Blocking Corrections Using the Velocity-ratio Method

Rectangular-wind-tunnel Blocking Corrections Using the Velocity-ratio Method PDF Author: Rudolph W. Hensel
Publisher:
ISBN:
Category : Mathematical analysis
Languages : en
Pages : 708

Book Description
Calculations of the ratios of the velocity increments at test bodies to those at the tunnel walls caused by the solid blocking of these bodies within the walls of a closed rectangular wind tunnel are presented. The boides treated include two-dimensional airfoils; small bodies of revolution; straight, untapered, finite-span wings of varying span; and swept, untapered, finite-span wings of varying span. It is shown that, after wake blocking effects have been removed , the present method furnishes semiempirical blocking corrections for most wind-tunnel models and their components. The test section proportions of the Southern California Cooperative Wind Tunnel at CIT (ratio of height to width equal to 1/square root of 2) are used in the calculations.

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 : 876

Book Description


Catalog of Technical Reports

Catalog of Technical Reports PDF Author: United States. Dept. of Commerce. Office of Technical Services
Publisher:
ISBN:
Category :
Languages : en
Pages : 742

Book Description


United States Government Publications Monthly Catalog

United States Government Publications Monthly Catalog PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1322

Book Description


Catalogue of Publications Issued by the Government of the United States

Catalogue of Publications Issued by the Government of the United States PDF Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1014

Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index

List of Technical Notes, 1947-1953

List of Technical Notes, 1947-1953 PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 162

Book Description


Elevated-temperature Properties of Several Titanium Carbide Base Ceramals

Elevated-temperature Properties of Several Titanium Carbide Base Ceramals PDF Author: George C. Deutsch
Publisher:
ISBN:
Category : Carbides
Languages : en
Pages : 56

Book Description
On a strength-to-weight ratio basis, ceramals appeared promising as gas-turbine-blade materials in the temperature range of 1600 to 2400 degrees F.

Aerodynamic Properties of Cruciform-wing and Body Combinations at Subsonic, Transonic, and Supersonic Speeds

Aerodynamic Properties of Cruciform-wing and Body Combinations at Subsonic, Transonic, and Supersonic Speeds PDF Author: John R. Spreiter
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 646

Book Description
The aerodynamic forces and moments exerted on pitched and yawed wing-body combinations consisting of a slender body of revolution and a cruciform arrangement of thin wings have been investigated by two theoretical methods. One method, an extension of the slender wing-body theory of NACA TN No. 1662, makes possible the determination of simple closed expressions for the load distribution, of simple closed expressions for the load distribution, the forces, and the moments for slender cruciform-wing and body combinations in which the wings may be dissimilar plan form. The second method treats cruciform-wing and body combinations consisting of a body of revolution and identical wings of arbitrary aspect ratio and plan form. The results are valid at subsonic, transonic, and supersonic speeds.

Report

Report PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 620

Book Description