A Wind-tunnel Test Technique for Measuring the Dynamic Rotary Stability Derivatives Including the Cross Derivatives at High Mach Numbers

A Wind-tunnel Test Technique for Measuring the Dynamic Rotary Stability Derivatives Including the Cross Derivatives at High Mach Numbers
Author :
Publisher :
Total Pages : 44
Release :
ISBN-13 : UOM:39015086496331
ISBN-10 :
Rating : 4/5 ( Downloads)

Book Synopsis A Wind-tunnel Test Technique for Measuring the Dynamic Rotary Stability Derivatives Including the Cross Derivatives at High Mach Numbers by : Benjamin H. Beam

Download or read book A Wind-tunnel Test Technique for Measuring the Dynamic Rotary Stability Derivatives Including the Cross Derivatives at High Mach Numbers written by Benjamin H. Beam and published by . This book was released on 1955 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is described for measuring the dynamic stability derivatives of a model airplane in a wind tunnel. The characteristics features of this system are that single-degree-of-freedom oscillations were used to obtain combinations of rolling, yawing, and pitching motions; that the oscillations were excited and controlled by velocity feedback which permitted operation under conditions unfavorable for more conventional types of oscillatory testing; and that data processing was greatly simplified by using analog computer elements in the strain-gage circuitry.


A Wind-tunnel Test Technique for Measuring the Dynamic Rotary Stability Derivatives Including the Cross Derivatives at High Mach Numbers Related Books

A Wind-tunnel Test Technique for Measuring the Dynamic Rotary Stability Derivatives Including the Cross Derivatives at High Mach Numbers
Language: en
Pages: 44
Authors: Benjamin H. Beam
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1955 - Publisher:

DOWNLOAD EBOOK

A method is described for measuring the dynamic stability derivatives of a model airplane in a wind tunnel. The characteristics features of this system are that
NASA Technical Note
Language: en
Pages: 528
Authors:
Categories:
Type: BOOK - Published: 1972 - Publisher:

DOWNLOAD EBOOK

Technical Note - National Advisory Committee for Aeronautics
Language: en
Pages: 600
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1954 - Publisher:

DOWNLOAD EBOOK

Prediction of Downwash Behind Swept-wing Airplanes at Subsonic Speed
Language: en
Pages: 688
Authors: John DeYoung
Categories: Airplanes
Type: BOOK - Published: 1955 - Publisher:

DOWNLOAD EBOOK

A rapid method for estimating the downwash behind swept-wing airplanes is presented. The basic assumption is that of a flat horizontal sheet of vortices trailin
U.S. Government Research Reports
Language: en
Pages: 48
Authors:
Categories: Science
Type: BOOK - Published: 1955 - Publisher:

DOWNLOAD EBOOK