An Investigation of the Low-speed Longitudinal Stability Characteristics of a Swept-wing Airplane Model with Two Modifications to the Wing-root Plan Form
Title | An Investigation of the Low-speed Longitudinal Stability Characteristics of a Swept-wing Airplane Model with Two Modifications to the Wing-root Plan Form PDF eBook |
Author | William B.Jr Kemp |
Publisher | |
Pages | 17 |
Release | 1952 |
Genre | |
ISBN |
Index of NACA Technical Publications
Title | Index of NACA Technical Publications PDF eBook |
Author | United States. National Advisory Committee for Aeronautics |
Publisher | |
Pages | 580 |
Release | 1956 |
Genre | Aeronautics |
ISBN |
Some Low-speed Wind-tunnel Experiments Pertaining to the Longitudinal Stability Characteristics of a 35© Swept-wing Model and an Unswept-wing Model
Title | Some Low-speed Wind-tunnel Experiments Pertaining to the Longitudinal Stability Characteristics of a 35© Swept-wing Model and an Unswept-wing Model PDF eBook |
Author | Byron M. Jaquet |
Publisher | |
Pages | 48 |
Release | 1953 |
Genre | Airplanes |
ISBN |
Effect of Wing Modifications on the Longitudinal Stability of a Tailless All-wing Airplane Model
Title | Effect of Wing Modifications on the Longitudinal Stability of a Tailless All-wing Airplane Model PDF eBook |
Author | Charles L. Seacord |
Publisher | |
Pages | 30 |
Release | 1945 |
Genre | Aerodynamics |
ISBN |
Summary: An investigation of the power-off longitudinal stability characteristics of a tailless all-wing airplane model with various wing modifications has been made in the Langley free-flight tunnel. Force and tuft tests were made on the model in the original condition, with the wing tips rotated for washout, with rectangular and swept-forward tips, and with various slat arrangements. Flight tests were made with the original wing and with the original wing equipped with the most promising modifications. The results indicated that changes in tip plan form or rotation of the wing tips did not appreciably reduce the instability at high lift coefficients. Addition of wing slats, however, improved the longitudinal stability at the stall when the slat extended far enough inboard to cover the area that tended to stall first.
Monthly Catalog of United States Government Publications
Title | Monthly Catalog of United States Government Publications PDF eBook |
Author | United States. Superintendent of Documents |
Publisher | |
Pages | 2106 |
Release | 1959 |
Genre | Government publications |
ISBN |
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.
Effects of Wing Inboard Plan-form Modifications on Lift, Drag, and Longitudinal Stability at Mach Numbers from 1.0 to 2.3 of a Rocket-propelled Free-flight Model with a 52.5 Degree Sweptback Wing of Aspect Ratio 3
Title | Effects of Wing Inboard Plan-form Modifications on Lift, Drag, and Longitudinal Stability at Mach Numbers from 1.0 to 2.3 of a Rocket-propelled Free-flight Model with a 52.5 Degree Sweptback Wing of Aspect Ratio 3 PDF eBook |
Author | Allen B. Henning |
Publisher | |
Pages | 32 |
Release | 1957 |
Genre | Aerofoils |
ISBN |
An investigation was made to determine the effects of wing inboard plan-form modifications on the lift, drag, and longitudinal characteristics of a rocket-propelled free-flight model. The model had a body of fineness ration 17.4, a modified wing with a basic plan form swept back 52.5 degrees and an aspect ratio of 3, and inline horizontal tail surfaces which were aerodynamically pulsed continuously throughout the flight.
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 | 750 |
Release | 1949 |
Genre | Aeronautics |
ISBN |