Author: Albin O. PearsonPublisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 74
Book Description
Wind-tunnel Investigation at Mach Numbers from 0.40 to 1.20 of the Static Aerodynamic and Control Characteristics of a Model of a Nonlifting Reeintry Capsule in Combination with a Rocket Booster
Author: Albin O. PearsonPublisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 74
Book Description
Wind-tunnel Investigation at Mach Numbers from 0.20 to 1.17 of the Static Aerodynamic Characteristics of a Possible Reentry Capsule
Author: Wind-tunnel Investigation at Mach Numbers from 0.40 to 1.14 of the Static Aerodynamic Characteristics of a Nonlifting Vehicle Suitable for Reentry
Author: Albin O. PearsonPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 14
Book Description
Wind Tunnel Investigation at Mach Numbers from 0.20 to 1.17 of the Static Aerodynamic Characterictics of a Possible Reentry Capsule
Author: Albin O. PearsonWind-tunnel Investigation at Mach Numbers from 1.60 to 4.50 of the Static-stability Characteristics of Two Nonlifting Vehicles Suitable for Reentry
Author: Kenneth L. TurnerInvestigation of Aerodynamic Effects of External Combustion Below Flat-plate Model in 10- by 10-foot Wind Tunnel at Mach 2.4
Author: Robert G. DorschPublisher:
ISBN:
Category : Mach number
Languages : en
Pages : 30
Book Description
Wind-tunnel Investigation at a Mach Number of 2.91 of Stability and Control Characteristics of Three Lifting Reentry Configurations at Angles of Attack Up to 90 Degrees
Author: Wind Tunnel Measurements of Hysteresis in the Static Aerodynamic Characteristics of Aircraft
Author: J. F. HermanPublisher:
ISBN:
Category : Hysteresis
Languages : en
Pages : 112
Book Description
Wind Tunnel Tests of Rectangular Finned Variable Gap Tangent Ogive-cylinder Model at Mach Numbers 1.75 to 4.50
Author: Neil Arthur ZarinPublisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 106
Book Description
Author: