Effects of Wing-crank, Leading-edge Chord Extensions and Horizontal-tail Height on the Longitudinal Stability of Swept-wing Models at Mach Numbers from 0.6 to 1.4 PDF Download

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Effects of Wing-crank, Leading-edge Chord Extensions and Horizontal-tail Height on the Longitudinal Stability of Swept-wing Models at Mach Numbers from 0.6 to 1.4

Effects of Wing-crank, Leading-edge Chord Extensions and Horizontal-tail Height on the Longitudinal Stability of Swept-wing Models at Mach Numbers from 0.6 to 1.4 PDF Author: Roy M. Wakefield
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 120

Book Description

Effects of Wing-crank, Leading-edge Chord Extensions and Horizontal-tail Height on the Longitudinal Stability of Swept-wing Models at Mach Numbers from 0.6 to 1.4

Effects of Wing-crank, Leading-edge Chord Extensions and Horizontal-tail Height on the Longitudinal Stability of Swept-wing Models at Mach Numbers from 0.6 to 1.4 PDF Author: Roy M. Wakefield
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 120

Book Description

Index of NASA Technical Publications

Index of NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448

Book Description

Scientific and Technical Aerospace Reports

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Category : Aeronautics
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Index to NASA Technical Publications

Index to NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
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Category :
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A Selected Listing of NASA Scientific and Technical Reports for ...

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Category : Government publications
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Category : Government publications
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Book Description

Some Effects of Tail Height and Wing Plan Form on the Static Longitudinal Stability Characteristics of a Small-scale Model at High Subsonic Speeds

Some Effects of Tail Height and Wing Plan Form on the Static Longitudinal Stability Characteristics of a Small-scale Model at High Subsonic Speeds PDF Author: Albert G. Few
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 80

Book Description
The drag due to lift increases with increasing sweep through the Mach number range. Some increase in bag due to lift is evident decrease in taper ratio for wings having 300of sweep through most of the speed range.
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