Force, Moment, and Flow-field Characteristics of Two Wing-body-nacelle Combinations at Mach Numbers 2 and 3
Author: Hill, Jr. (William A.)
Publisher:
Published: 1960
Total Pages: 102
ISBN-13:
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Author: Hill, Jr. (William A.)
Publisher:
Published: 1960
Total Pages: 102
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1960
Total Pages: 96
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DOWNLOAD EBOOKAuthor: United States. Superintendent of Documents
Publisher:
Published: 1959
Total Pages: 1714
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DOWNLOAD EBOOKFebruary issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
Author:
Publisher:
Published: 1992
Total Pages: 1572
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DOWNLOAD EBOOKAuthor: Lyndell S. King
Publisher:
Published: 1973
Total Pages: 132
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DOWNLOAD EBOOKWind tunnel tests were conducted to determine the flow distribution about fuselage configurations at transonic and supersonic speeds and at angles of attack up to 20 degrees. The models tested were approximately one-twelfth scale and consisted of a main fuselage forebody member and several attachable components. The components were mounted in several combinations to represent different possible configurations for tactical aircraft. Flow distribution surveys were conducted at two inlet locations ahead of and under the wing to assess the effects of forebody geometry for the conditions indicated. The data indicate the influence of the canopy, nose droop, and fuselage shape on flow angularities in the forward survey plane.
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
Published: 1966
Total Pages: 1440
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Published: 1954
Total Pages: 818
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DOWNLOAD EBOOKAuthor: Dale E. Knutsen
Publisher:
Published: 1968
Total Pages: 72
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DOWNLOAD EBOOKAuthor: Harry W. Carlson
Publisher:
Published: 1959
Total Pages: 78
ISBN-13:
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