Author: P. J. RauhutPublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Propeller Slipstream Effects on Lateral and Directional Static Stability and Control of a Single Engine Traction Airplane
Author: P. J. RauhutLateral Stability and Control Characteristics of a Four-propeller Deflected-slipstream VTOL Model Including the Effects of Ground Proximity
Author: Richard E. KuhnPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 76
Book Description
Tests to Determine Effects of Slipstream Rotation on the Lateral Stability Characteristics of a Single-engine Low-wing Airplane Model
Author: Paul E. PurserPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 20
Book Description
Tests have been made of a 1/5-scale powered model of a single-engine low-wing airplane with three propeller-blade settings and three values of tail length to provide information on the effects of slipstream rotation on the directional stability and control characteristics of single-engine airplanes.
A Method for the Determination of the Effect of Propeller Slipstream on the Static Longitudinal Stability and Control of Multi-engined Aircraft
Author: E. ObertPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 286
Book Description
The Effect on Stability and Control of a Pusher Propeller Behind Conventional Tail Surfaces as Determined by Tests of a Powered Model in the Free-flight Tunnel
Author: John P. CampbellPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 56
Book Description
Summary: The effects on stability and control of a pusher propeller behind conventional horizontal and vertical tail surfaces have been determined in the NACA free-flight tunnel by tests of a 1/10-scale model of an NACA submerged-engine pusher airplane design. The investigation consisted of flight and balance tests at windmilling and high-power conditions with a partial-span Zap extensible flap extended and retracted. The effects of changes in vertical-tail area, horizontal-tail incidence, and center-of-gravity location were also determined.
A Flight Investigation of the Performance, Handling Qualities, and Operational Characteristics of a Deflected Slipstream STOL Transport Airplane Having Four Interconnected Propellers
Author: Hervey C. QuigleyPublisher:
ISBN:
Category : Propellers, Aerial
Languages : en
Pages : 70
Book Description
Lateral Control Characteristics of a Powered Model of a Twin-propeller Deflected Slipstream STOL Airplane Configuration
Author: Richard J. MargasonPublisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 208
Book Description
A Method for the Determination of the Effect of Propeller Slipstream on Static Longitudinal Stability and Control of Multi-engined Aircraft
Author: E. ObertPublisher:
ISBN: 9789056230098
Category :
Languages : en
Pages : 54
Book Description
Lateral Stability and Control Characteristics of a Four-Propeller Deflected-Slipstream VTOL Model Including the Effects of Ground Proximity
Author: Effects of an In-flight Thrust Reverser on the Stability and Control Characteristics of a Single-engine Fighter Airplane Model
Author: Charles E. MercerPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 244
Book Description
The changes in thrust minus drag performance as well as longitudinal and directional stability and control characteristics of a single-engine jet aircraft attributable to an in-flight thrust reverser of the blocker-deflector door type were investigated in a 16-foot transonic wind tunnel. The longitudinal and directional stability data are presented. Test conditions simulated landing approach conditions as well as high speed maneuvering such as may be required for combat or steep descent from high altitude.