Author: H. Norman Silvers
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 22
Book Description
The results presented in this paper indicate that the effects of stores on wing load distribution at subsonic speeds may be predicted by available methods at the lower angles of attack where wing flow separation is negligible. At the higher angles of attack where wing flow separation exists, a store located inboard on a swept wing may act much like various devices designed to delay wing pitch-up by reducing the loss in load at the wing tip due to flow separation. Furthermore, the results indicate that the normal force and pitching moment of a store located at the wing tip can be calculated quite well by available methods. On the other hand, no theoretical procedure is available to calculate the severe lateral forces and moments encountered at zero sideslip on an inboard arrangement of stores on a swept wing.
Some Notes on the Aerodynamic Loads Associated with External-store Installations
Author: H. Norman Silvers
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 22
Book Description
The results presented in this paper indicate that the effects of stores on wing load distribution at subsonic speeds may be predicted by available methods at the lower angles of attack where wing flow separation is negligible. At the higher angles of attack where wing flow separation exists, a store located inboard on a swept wing may act much like various devices designed to delay wing pitch-up by reducing the loss in load at the wing tip due to flow separation. Furthermore, the results indicate that the normal force and pitching moment of a store located at the wing tip can be calculated quite well by available methods. On the other hand, no theoretical procedure is available to calculate the severe lateral forces and moments encountered at zero sideslip on an inboard arrangement of stores on a swept wing.
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 22
Book Description
The results presented in this paper indicate that the effects of stores on wing load distribution at subsonic speeds may be predicted by available methods at the lower angles of attack where wing flow separation is negligible. At the higher angles of attack where wing flow separation exists, a store located inboard on a swept wing may act much like various devices designed to delay wing pitch-up by reducing the loss in load at the wing tip due to flow separation. Furthermore, the results indicate that the normal force and pitching moment of a store located at the wing tip can be calculated quite well by available methods. On the other hand, no theoretical procedure is available to calculate the severe lateral forces and moments encountered at zero sideslip on an inboard arrangement of stores on a swept wing.
External Store Airloads Prediction Technique
Author: A. R. Rudnicki (Jr.)
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 170
Book Description
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 170
Book Description
NASA Technical Note
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 864
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 864
Book Description
Determination of Captive Flight Loads and Separation Trajectories of Airborne Stores
Author: Dale E. Knutsen
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 72
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 72
Book Description
A Summary of NASA Data Relative to External-store Separation Characteristics
Author: Linwood W. McKinney
Publisher:
ISBN:
Category : Bomb racks
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Bomb racks
Languages : en
Pages : 28
Book Description
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 860
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 860
Book Description
Missile Configuration Design
Author: S. S. Chin
Publisher:
ISBN:
Category : Guided missiles
Languages : en
Pages : 304
Book Description
Beskriver principperne i f.m. konstruktionen af styrede missiler.
Publisher:
ISBN:
Category : Guided missiles
Languages : en
Pages : 304
Book Description
Beskriver principperne i f.m. konstruktionen af styrede missiler.
NACA Conference on Aircraft Loads, Structures, and Flutter
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 702
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 702
Book Description
Technique Development for Predicting External Store Aerodynamic Effects on Aircraft Performance
Author: R. Dale Gallagher
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 470
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 470
Book Description
Research Abstracts
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 442
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 442
Book Description