Author: Windsor L. ShermanPublisher:
ISBN:
Category : Aircraft accidents
Languages : en
Pages : 60
Book Description
An Analytical Study of the Longitudinal Response of Airplanes to Positive Wind Shear
Author: Windsor L. ShermanPublisher:
ISBN:
Category : Aircraft accidents
Languages : en
Pages : 60
Book Description
An Analytical Study of the Longitudinal Response of Airplanes to Positive Wind Shear
Author: Windsor L. ShermanPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 60
Book Description
A theoretical analysis of airplane longitudinal stability and control as affected by wind shear
Author: Windsor L. ShermanPublisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 62
Book Description
NASA Technical Paper
Author: Scientific and Technical Aerospace Reports
Author: NASA Scientific and Technical Publications
Author: Monthly Catalog, United States Public Documents
Author: United States. Superintendent of DocumentsPublisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1716
Book Description
February 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
LARCMACS: A TEX Macro Set for Typesetting NASA Reports
Author: Calculation of Vertical and Ramp-assisted Takeoffs for Supersonic Cruise Fighters
Author: Analytical Study of the Effect of Center-of-gravity Position on the Response to Longitudinal Control in Landing Approaches of a Swept-wing Airplane of Low Aspect Ratio Having No Horizontal Tail
Author: Ralph W. StonePublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 35
Book Description
An analytical study of the short-time response characteristics to longitudinal control moments of a swept-wing airplane of low aspect ratio having no horizontal tail has indicated that difficulty reported in landings aboard an aircraft carrier may have been the result of a relatively larger time lag in the response of the airplane in changing its flight-path angle than exists on more conventional type airplanes. It has been reasoned that reduction of the airplane's static longitudinal stability might improve the response characteristics. Accordingly, an analytical study of the effect of reducing the static stability by a practical center-of-gravity shift has been made.