Author: Langley Aeronautical Laboratory
Publisher: Hassell Street Press
ISBN: 9781014962751
Category :
Languages : en
Pages : 104
Book Description
This work has been selected by scholars as being culturally important and is part of the knowledge base of civilization as we know it. This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. To ensure a quality reading experience, this work has been proofread and republished using a format that seamlessly blends the original graphical elements with text in an easy-to-read typeface. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
Effect of High Wing Loading on Landing Technique and Distance, With Experimental Data for the B-26 Airplane
Author: Langley Aeronautical Laboratory
Publisher: Hassell Street Press
ISBN: 9781014962751
Category :
Languages : en
Pages : 104
Book Description
This work has been selected by scholars as being culturally important and is part of the knowledge base of civilization as we know it. This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. To ensure a quality reading experience, this work has been proofread and republished using a format that seamlessly blends the original graphical elements with text in an easy-to-read typeface. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
Publisher: Hassell Street Press
ISBN: 9781014962751
Category :
Languages : en
Pages : 104
Book Description
This work has been selected by scholars as being culturally important and is part of the knowledge base of civilization as we know it. This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. To ensure a quality reading experience, this work has been proofread and republished using a format that seamlessly blends the original graphical elements with text in an easy-to-read typeface. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
The Effect of High Wing Loading on Landing Technique and Distance, with Experimental Data for the B-26 Airplane
Author: F. B. Gustafson
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 112
Book Description
1. Considerations of safety and accuracy limit the rate of descent used in the landing approach to about 25 feet per second.
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 112
Book Description
1. Considerations of safety and accuracy limit the rate of descent used in the landing approach to about 25 feet per second.
Wartime Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 400
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 400
Book Description
Wartime Report
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
NACA Wartime Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 712
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 712
Book Description
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 616
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 616
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664
Book Description
Index of NACA Reports Having Application to Personal Aircraft
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
Book Description
NACA Conference on Some Problems of Aircraft Operation
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 332
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 332
Book Description
Effect of Ice and Frost Formations on Drag of NACA 651-212 Airfoil for Various Modes of Thermal Ice Protection
Author: Vernon H. Gray
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 720
Book Description
The effects of primary and runback icing and frost formations on the drag of an 8-foot-chord NACA 651-212 airfoil section were investigated over a range of angles of attack from 2 degrees to 8 degrees and airspeeds up to 260 miles per hour for icing conditions with liquid-water contents ranging from 0.25 to 1.4 grams per cubic meter and datum air temperatures of -30 to 30 degrees F.
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 720
Book Description
The effects of primary and runback icing and frost formations on the drag of an 8-foot-chord NACA 651-212 airfoil section were investigated over a range of angles of attack from 2 degrees to 8 degrees and airspeeds up to 260 miles per hour for icing conditions with liquid-water contents ranging from 0.25 to 1.4 grams per cubic meter and datum air temperatures of -30 to 30 degrees F.