Charts for Calculating the Performance of Airplanes Having Constant-speed Propellers PDF Download
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Author: Roland J. White
Publisher:
ISBN:
Category : Aeronautical charts
Languages : en
Pages : 580
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Book Description
Examples applying the charts to airplanes having both supercharged and unsupercharged engines are included.
Author: Roland J. White
Publisher:
ISBN:
Category : Aeronautical charts
Languages : en
Pages : 580
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Book Description
Examples applying the charts to airplanes having both supercharged and unsupercharged engines are included.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 634
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 616
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 792
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Book Description
Author: John T. Lowry
Publisher: AIAA
ISBN: 9781563473302
Category : Mathematics
Languages : en
Pages : 508
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Book Description
Pilots, aviation students, kitplane builders, aircraft fleet operators and aeronautical engineers can all determine how their propeller-driven airplanes will perform, under any conditions, by using the step-by-step bootstrap approach introduced in this book. A few routine flying manoeuvres (climbs, glides, a level speed run) will give the necessary nine numbers. High-school level calculations then give performance numbers with much greater detail and accuracy than many other methods - for the reader's individual aircraft.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :
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Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 760
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Book Description
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 654
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Book Description
Author: Ira H. A. Abbott
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 576
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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.
Author: Clifford J. Moore
Publisher:
ISBN:
Category :
Languages : en
Pages : 492
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Book Description
