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Flight Measurements of Stability and Control Derivatives of the X-15 Research Airplane to a Mach Number of 6.02 and an Angle of Attack of 250

Roxanah B. Yancey

Published: 1964

Total Pages: 56

Flight Measurements of Stability and Control Derivatives of the X-15 Research Airplane to a Mach Number of 6.02 and an Angle of Attack of 25 Degrees

Roxannah B. Yancey

Published: 1964

Total Pages: 47

Flight Measurements of Stability and Control Derivatives of the X-15 Research Airplane to a Mach Number of 6.02 and an Angle of Attack of 25°

Roxanah B. Yancey

Published: 1964

Total Pages: 47

Aerodynamic-derivative Characteristics of the X-15 Research Airplane as Determined from Flight Tests for Mach Numbers from 0.6 to 3.4

Roxanah B. Yancey

Published: 1962

Total Pages: 72

Aerodynamic and Landing Measurements Obtained During the First Powered Flight of the North American X-15 Research Airplane

Published: 1960

Total Pages: 44

Flight Behavior of the X-2 Research Airplane to a Mach Number of 3.20 and a Geometric Altitude of 126,200 Feet

Richard E. Day

Published: 1959

Total Pages: 26

Static Longitudinal, Directional, and Lateral Stability and Control Data at a Mach Number of 6.83 of the Final Configuration of the X-15 Research Airplane

Jim A. Penland

Published: 1960

Total Pages: 150

Stability and Control Characteristics of a 0.0667-scale Model of the Final Version of the North American X-15 Research Airplane (configuration 3) at Transonic Speeds

Robert S. Osborne

Published: 1963

Total Pages: 112

Investigation of the Subsonic Stability and Control Characteristics of a 1/7-scale Model of the North American X-15 Airplane with and Without Fuselage Forebody Strakes

James L. Hassell

Published: 1960

Total Pages: 52

Subsonic Flight Tests of a 1/7-scale Radio-controlled Model of the North American X-15 Airplane with Particular Reference to High Angle-of-attack Conditions

Donald E. Hewes

Published: 1960

Total Pages: 48