Effect At High Subsonic Speeds Of Fuselage Forebody Strakes On The Static Stability And Vertical Tail Load Characteristics Of A Complete Model Having A Delta Wing PDF Download

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Effect at High Subsonic Speeds of Fuselage Forebody Strakes on the Static Stability and Vertical-tail-load Characteristics of a Complete Model Having a Delta Wing

Effect at High Subsonic Speeds of Fuselage Forebody Strakes on the Static Stability and Vertical-tail-load Characteristics of a Complete Model Having a Delta Wing
Author: Edward C. Polhamus
Publisher:
Total Pages: 36
Release: 1958
Genre: Airplanes
ISBN:

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A wind-tunnel investigation at high subsonic speeds has been conducted to determine the effect of fuselage forebody strakes on the static stability and the vertical-tail-load characteristics of an airplane-type configuration having a delta wing. The tests were made at Mach numbers from 0.60 to 0.92 corresponding to Reynolds numbers from 3,000,000 to 4,200,000, based on the wing mean aerodynamic chord, and at angles of attack from approximately -2 to 24 degrees.


NASA Technical Note

NASA Technical Note
Author:
Publisher:
Total Pages: 560
Release: 1961
Genre:
ISBN:

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Applied Mechanics Reviews

Applied Mechanics Reviews
Author:
Publisher:
Total Pages: 1116
Release: 1962
Genre: Mechanics, Applied
ISBN:

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Index of NACA Technical Publications

Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 860
Release: 1957
Genre: Aeronautics
ISBN:

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Index of NASA Technical Publications

Index of NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
Total Pages: 448
Release: 1960
Genre: Aeronautics
ISBN:

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