Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1958
Total Pages: 48
ISBN-13:
DOWNLOAD EBOOKPosts
Experimental Determination of Effects of Frequency and Amplitude on the Lateral Stability Derivatives for a Delta, a Swept, and an Upswept Wing Oscillating in Yaw
Author: Dean R. Chapman
Publisher:
Published: 1958
Total Pages: 206
ISBN-13:
DOWNLOAD EBOOKTechnical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1957
Total Pages: 878
ISBN-13:
DOWNLOAD EBOOKExperimental Investigation of the Effect of Vertical-tail Size and Length and of Fuselage Shape and Length on the Static Lateral Stability Characteristics of a Model with 45 ̊sweptback Wing and Tail Surfaces
Author: Antonio Ferri
Publisher:
Published: 1951
Total Pages: 328
ISBN-13:
DOWNLOAD EBOOKHigh Speed Problems of Aircraft and Experimental Methods
Author: Allen F. Donovan
Publisher: Princeton University Press
Published: 2015-12-08
Total Pages: 1021
ISBN-13: 140087503X
DOWNLOAD EBOOKVolume VIII of the High Speed Aerodynamics and Jet Propulsion series. This volume includes: performance calculation at high speed; stability and control of high speed aircraft; aeroelasticity and flutter; model testing; transonic wind tunnels; supersonic tunnels; hypersonic experimental facilities; low density wind tunnels; shock tube; wind tunnel measurements; instrumented models in free flight; piloted aircraft testing; free flight range methods. Originally published in 1961. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Research Abstracts
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1952
Total Pages: 16
ISBN-13:
DOWNLOAD EBOOKAnnual Report of the National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Published:
Total Pages: 872
ISBN-13:
DOWNLOAD EBOOKIndex of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1956
Total Pages: 580
ISBN-13:
DOWNLOAD EBOOKWind-tunnel Investigation to Determine the Horizontal- and Vertical-tail Contributions to the Static Lateral Stability Characteristics of a Complete-model Swept-wing Configuration at High Subsonic Speeds
Author: James W. Wiggins
Publisher:
Published: 1956
Total Pages: 692
ISBN-13:
DOWNLOAD EBOOKAn investigation was conducted in the Langley high-speed 7- by 10-foot tunnel to determine the horizontal- and vertical-tail contributions to the static lateral stability of a complete-model swept-wing configuration at high subsonic speeds. The results indicate that, in a general, Mach number effects within the range studied and wing effects on the tail contribution were small and the overall trends of the data of the present investigation agreed with those which have been established at low speeds.
