Author: William A. Corlett
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description
Lateral Directional Stability Characteristics at Mach 2.3 to 3.5 of a Supersonic Transport Model with Various Outboard Vertical-tail Locations
Supersonic Lateral-directional Stability Characteristics of a 45 ̊swept Wing-body-tail Model with Various Body Cross-sectional Shapes
Author: Dennis E. Fuller
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 54
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 54
Book Description
High-lift Characteristics of a Variable-sweep Supersonic Transport Model with a Blended Engine-fuselage and Engine-mounted Horizontal Tails
Experimental and Theoretical Supersonic Lateral-directional Stability Characteristics of a Simplified Wing-body Configuration with a Series of Vertical-tail Arrangements
Author: Milton Lamb
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 50
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 50
Book Description
Aerodynamic Characteristics at Mach Numbers 2.30, 2.60, and 2.96 of a Supersonic Transport Model Having a Fixed, Warped Wing
Theoretical and Experimental Supersonic Lateral-Directional Stability Characteristics
Author: Milton Lamb
Publisher:
ISBN:
Category :
Languages : en
Pages : 8
Book Description
A program has been initiated at NASA Langley Research Center to assess several methods for estimation of lateral-directional stability. As a basis for comparison, experimental data are presented for a simple wing-body vertical tail configuration. The methods for estimating the characteristics include a second-order shock expansion and panel method (MISLIFT), a slender body and 'first-order' panel method (APAS), and a 'higher-order' panel method for linearized supersonic flow (PAN AIR). The results show that PAN AIR provides accurate estimates of these characteristics at moderate angles of attack for complete configurations with either single or twin vertical tails. APAS will provide estimates for complete configurations at zero angle of attack. However, MISLIFT will only provide estimates for the simplest body-vertical tail configurations at zero angle of attack. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 8
Book Description
A program has been initiated at NASA Langley Research Center to assess several methods for estimation of lateral-directional stability. As a basis for comparison, experimental data are presented for a simple wing-body vertical tail configuration. The methods for estimating the characteristics include a second-order shock expansion and panel method (MISLIFT), a slender body and 'first-order' panel method (APAS), and a 'higher-order' panel method for linearized supersonic flow (PAN AIR). The results show that PAN AIR provides accurate estimates of these characteristics at moderate angles of attack for complete configurations with either single or twin vertical tails. APAS will provide estimates for complete configurations at zero angle of attack. However, MISLIFT will only provide estimates for the simplest body-vertical tail configurations at zero angle of attack. (Author).
Experimental and Theoretical Supersonic Lateral-directional Stability Characteristics of a Simplified Wing-body Configuration with a Series of Vertical-tail Arrangements
Author: Milton Lamb
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 52
Book Description