Lift Developed on Unrestrained Rectangular Wings Entering Gusts at Subsonic and Supersonic Speeds

Lift Developed on Unrestrained Rectangular Wings Entering Gusts at Subsonic and Supersonic Speeds PDF Author: Harvard Lomax
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 50

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Book Description
The object of this report is to provide an estimate, based on theoretical calculations, of the forces induced on a wing that is flying at a constant forward speed and suddenly enters a vertical gust. The calculations illustrate the effects of Mach number (from 0 to 2) and aspect ration (2 to infinity), and solutions are given by means of which the response to gusts having arbitrary distributions of velocity can be calculated. The effects of pitching and wing bending are neglected and only wings of rectangular plan form are considered. Specific results are presented for sharp-edged and triangular gusts and various wing-air density ratios.

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 :

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

Annual Report

Annual Report PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 534

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Report - National Advisory Committee for Aeronautics

Report - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702

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Report

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

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Method for Calculating the Rolling and Yawing Moments Due to Rolling for Unswept Wings with Or Without Flaps Or Ailerons by Use of Nonlinear Section Lift Data

Method for Calculating the Rolling and Yawing Moments Due to Rolling for Unswept Wings with Or Without Flaps Or Ailerons by Use of Nonlinear Section Lift Data PDF Author: Albert P. Martina
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ISBN:
Category : Aeronautics
Languages : en
Pages : 274

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Unsteady Aerodynamic Forces on Subsonic Aircraft Exposed to Blast Gusts of Arbitrary Orientation

Unsteady Aerodynamic Forces on Subsonic Aircraft Exposed to Blast Gusts of Arbitrary Orientation PDF Author: Robert F. Smiley
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 108

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NASA's Contributions to Aeronautics: Flight environment, operations, flight testing, and research

NASA's Contributions to Aeronautics: Flight environment, operations, flight testing, and research PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1064

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Book Description
Two-volume collection of case studies on aspects of NACA-NASA research by noted engineers, airmen, historians, museum curators, journalists, and independent scholars. Explores various aspects of how NACA-NASA research took aeronautics from the subsonic to the hypersonic era.-publisher description.

NASA's Contributions to Aeronautics, Volume 2, Flight Environment ..., NASA/SP-2010-570-Vol 2, 2010, *

NASA's Contributions to Aeronautics, Volume 2, Flight Environment ..., NASA/SP-2010-570-Vol 2, 2010, * PDF Author:
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ISBN:
Category :
Languages : en
Pages : 1070

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WADC Technical Report

WADC Technical Report PDF Author: United States. Wright Air Development Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1268

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Book Description