Heat transfer from cylinders having closely spaced fins 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 Heat transfer from cylinders having closely spaced fins PDF full book. Access full book title Heat transfer from cylinders having closely spaced fins by Arnold E. Biermann. Download full books in PDF and EPUB format.

Heat transfer from cylinders having closely spaced fins

Heat transfer from cylinders having closely spaced fins PDF Author: Arnold E. Biermann
Publisher:
ISBN:
Category :
Languages : de
Pages : 74

Book Description

Heat transfer from cylinders having closely spaced fins

Heat transfer from cylinders having closely spaced fins PDF Author: Arnold E. Biermann
Publisher:
ISBN:
Category :
Languages : de
Pages : 74

Book Description

Heat Transfer from Cylinders Having Closely Spaced Fins

Heat Transfer from Cylinders Having Closely Spaced Fins PDF Author: Arnold E. Biermann
Publisher:
ISBN:
Category : Cylinders
Languages : en
Pages : 622

Book Description
The use of baffles for directing the air around the cylinders with closely spaced fins proved very effective in increasing the over-all heat-transfer coefficient provided that the spacing was not appreciably less than that for maximum heat transfer.

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 : 698

Book Description

Interference of Wing and Fuselage from Tests of 17 Combinations in the N.A.C.A. Variable-density Tunnel Combinations with Special Junctures

Interference of Wing and Fuselage from Tests of 17 Combinations in the N.A.C.A. Variable-density Tunnel Combinations with Special Junctures PDF Author: Albert Sherman
Publisher:
ISBN:
Category : Aiprlanes
Languages : en
Pages : 534

Book Description
As part of the wing-fuselage interferences investigation in progress in the N.A.C.A. variable-density wind tunnel, a method of eliminating the interference burble associated with critical midwing combinations was investigated. The interference burble of the critical midewing combination was shown to respond to modifications at the nose of the juncture and to be entirely suppressed with little or no adverse effect on the high-speed drag by special leading-edge fillets.

Annual Report - National Advisory Committee for Aeronautics

Annual Report - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :

Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 616

Book Description

Catalogue of the Public Documents of the ... Congress and of All Departments of the Government of the United States for the Period from ... to ...

Catalogue of the Public Documents of the ... Congress and of All Departments of the Government of the United States for the Period from ... to ... PDF Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 3208

Book Description

Catalogue of the Public Documents of the [the Fifty-third] Congress [to the 76th Congress] and of All Departments of the Government of the United States

Catalogue of the Public Documents of the [the Fifty-third] Congress [to the 76th Congress] and of All Departments of the Government of the United States PDF Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 3208

Book Description

Fuselage-drag Tests in the Variable-density Wind Tunnel

Fuselage-drag Tests in the Variable-density Wind Tunnel PDF Author: Ira H. A. Abbott
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 576

Book Description
Results are presented on drag tests of six bodies of revolution with systematically varying shapes and with a fineness ratio of 5. The formes were derived from source-sink distributions, and formulas are presented for the calculation of the pressure distributions of the forms. The tests were made in the N.A.C.A. variable-density tunnel over a range of values of Reynolds number from about 1,500,000 to 25,000,000. The results show that the bodies with the sharper noses and tails have the lowest drag coefficients are based on the two-thirds power of the volume. The data show the most important single characteristic of the body form to be the tail angle, which must be fine to obtain low drag.

Technical Note

Technical Note PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 42

Book Description

➤