Status of Spin Research for Recent Airplane Designs
Title | Status of Spin Research for Recent Airplane Designs PDF eBook |
Author | A. I. Neihouse |
Publisher | |
Pages | 60 |
Release | 1960 |
Genre | Airplanes |
ISBN |
The study is presented in terms of the following major problem areas: interpretation of results of spin-model research, analytical spin studies, techniques involved in obtaining measurements of various parameters in the spin, effectiveness of controls during spin and recoveries, influence of long noses, strakes, and canards on spin and recovery characteristics, and correlation of spin and recovery characteristics for recent airplane and model designs.
Status of Spin Research for Recent Airplane Designs
Title | Status of Spin Research for Recent Airplane Designs PDF eBook |
Author | A. I. Neihouse |
Publisher | |
Pages | 54 |
Release | 1960 |
Genre | Airplanes |
ISBN |
Status of Spin Research for Recent Airplane Designs
Title | Status of Spin Research for Recent Airplane Designs PDF eBook |
Author | |
Publisher | |
Pages | 98 |
Release | 1957 |
Genre | |
ISBN |
NASA Technical Report
Title | NASA Technical Report PDF eBook |
Author | |
Publisher | |
Pages | 308 |
Release | 1960 |
Genre | Aerodynamics |
ISBN |
Index of NASA Technical Publications
Title | Index of NASA Technical Publications PDF eBook |
Author | United States. National Aeronautics and Space Administration |
Publisher | |
Pages | 446 |
Release | 1961 |
Genre | Aeronautics |
ISBN |
A Selected Listing of NASA Scientific and Technical Reports for ...
Title | A Selected Listing of NASA Scientific and Technical Reports for ... PDF eBook |
Author | |
Publisher | |
Pages | 450 |
Release | 1960 |
Genre | Aeronautics |
ISBN |
Exploratory Wind-tunnel Investigation of Deployable Flexible Ventral Fins for Use as an Emergency Spin-recovery Device
Title | Exploratory Wind-tunnel Investigation of Deployable Flexible Ventral Fins for Use as an Emergency Spin-recovery Device PDF eBook |
Author | Sanger M. Burk |
Publisher | |
Pages | 48 |
Release | 1971 |
Genre | Aeronautics |
ISBN |
Spin-tunnel tests have been conducted on dynamic models of two fighter airplanes to explore the feasibility of using deployable flexible ventral fins as an emergency spin-recovery device. Various fin configurations, deflections, and locations were tested. The results indicated that the fins provided satisfactory spin recoveries for the models tested.