Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 644
Book Description
NACA Wartime Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 644
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 644
Book Description
NACA Wartime Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category :
Languages : en
Pages : 550
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 550
Book Description
List of NACA Wartime Reports
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 48
Book Description
Wartime Report
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 264
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 264
Book Description
List of NACA Reports Reprinted as Wartime Reports
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 44
Book Description
Wartime Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 342
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 342
Book Description
NACA Wartime Reports. Series L.
Author: Paul Kuhn
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 14
Book Description
Tests were made of a number of 10-inch shear panels of 24S-T aluminum alloy with 1- 1/2-inch holes to determine the stress concentrations at static rupture and the deformation characteristics. The average factor of stress concentration was found to be about 1.1; reinforcements around the edges of the holes did not increase the ultimate strengths. Permanent set began in specimens without holes at nominal shear stresses of 10 to 12 kips per square inch. In thin specimens with holes, permanent set began at the buckling stress.
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 14
Book Description
Tests were made of a number of 10-inch shear panels of 24S-T aluminum alloy with 1- 1/2-inch holes to determine the stress concentrations at static rupture and the deformation characteristics. The average factor of stress concentration was found to be about 1.1; reinforcements around the edges of the holes did not increase the ultimate strengths. Permanent set began in specimens without holes at nominal shear stresses of 10 to 12 kips per square inch. In thin specimens with holes, permanent set began at the buckling stress.
Wartime Report
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 746
Book Description
Reproductions of reports, some declassified, of research done at Aircraft Engine Research Laboratory during World War II. The order of reports does not represent when they were chronologically issued. Reference to the original version of each report is included.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 746
Book Description
Reproductions of reports, some declassified, of research done at Aircraft Engine Research Laboratory during World War II. The order of reports does not represent when they were chronologically issued. Reference to the original version of each report is included.
Wartime Report Release List
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category :
Languages : en
Pages : 200
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 200
Book Description
Wartime Report
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 550
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 550
Book Description