Longitudinal and Lateral Stability Characteristics of a 0.04-Scale Model of the Lockheed F-104a Airplane at Mach Numbers of 1.82 and 2.01. Coord. No. downloadPDF, EPUB, MOBI
Longitudinal and Lateral Stability Characteristics of a 0.04-Scale Model of the Lockheed F-104a Airplane at Mach Numbers of 1.82 and 2.01. Coord. No. downloadPDF, EPUB, MOBI
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Author: Nasa Technical Reports Server (Ntrs)
Number of Pages: 76 pages
Published Date: 23 Jul 2013
Publisher: Bibliogov
Publication Country: United States
Language: English
ISBN: 9781287236580
File Name: Longitudinal.and.Lateral.Stability.Characteristics.of.a.0.04-Scale.Model.of.the.Lockheed.F-104a.Airplane.at.Mach.Numbers.of.1.82.and.2.01..Coord..No..pdf
Download Link: Longitudinal and Lateral Stability Characteristics of a 0.04-Scale Model of the Lockheed F-104a Airplane at Mach Numbers of 1.82 and 2.01. Coord. No.
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An investigation has been made in the Langley 4 by 4-foot supersonic pressure tunnel at Mach numbers of 1.82 and 2.01 to determine the longitudinal and lateral static-stability characteristics of a 0.04-scale model of the Lockheed F-104A airplane. The effects of a modified vertical tail, several ventral-fin arrangements, and several external store arrangements were also determined. The tests were made at Reynolds numbers of 1.02 (exp 6) and 1.382 (exp 6), respectively, based on the wing mean geometric chord. The tests were made of combined angles of attack and sideslip that varied from about -4 deg. to about 20 deg.
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Longitudinal and Lateral Stability Characteristics of a 0.04-Scale Model of the Lockheed F-104a Airplane at Mach Numbers of 1.82 and 2.01. Coord. No. by Nasa Technical Reports Server (Ntrs)
Author: Nasa Technical Reports Server (Ntrs)
Number of Pages: 76 pages
Published Date: 23 Jul 2013
Publisher: Bibliogov
Publication Country: United States
Language: English
ISBN: 9781287236580
File Name: Longitudinal.and.Lateral.Stability.Characteristics.of.a.0.04-Scale.Model.of.the.Lockheed.F-104a.Airplane.at.Mach.Numbers.of.1.82.and.2.01..Coord..No..pdf
Download Link: Longitudinal and Lateral Stability Characteristics of a 0.04-Scale Model of the Lockheed F-104a Airplane at Mach Numbers of 1.82 and 2.01. Coord. No.
---------------------------------------------------------------
An investigation has been made in the Langley 4 by 4-foot supersonic pressure tunnel at Mach numbers of 1.82 and 2.01 to determine the longitudinal and lateral static-stability characteristics of a 0.04-scale model of the Lockheed F-104A airplane. The effects of a modified vertical tail, several ventral-fin arrangements, and several external store arrangements were also determined. The tests were made at Reynolds numbers of 1.02 (exp 6) and 1.382 (exp 6), respectively, based on the wing mean geometric chord. The tests were made of combined angles of attack and sideslip that varied from about -4 deg. to about 20 deg.
Read online Longitudinal and Lateral Stability Characteristics of a 0.04-Scale Model of the Lockheed F-104a Airplane at Mach Numbers of 1.82 and 2.01. Coord. No. Buy and read online Longitudinal and Lateral Stability Characteristics of a 0.04-Scale Model of the Lockheed F-104a Airplane at Mach Numbers of 1.82 and 2.01. Coord. No. Download and read Longitudinal and Lateral Stability Characteristics of a 0.04-Scale Model of the Lockheed F-104a Airplane at Mach Numbers of 1.82 and 2.01. Coord. No. for pc, mac, kindle, readers Download to iPad/iPhone/iOS, B&N nook Longitudinal and Lateral Stability Characteristics of a 0.04-Scale Model of the Lockheed F-104a Airplane at Mach Numbers of 1.82 and 2.01. Coord. No. ebook, pdf, djvu, epub, mobi, fb2, zip, rar, torrent
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