Static Aerodynamic Characteristics of a Model of a Horizontal-take-off Reusable Launch Vehicle at Mach Numbers 1.60, 2.16, and 2.86 PDF Download

Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Static Aerodynamic Characteristics of a Model of a Horizontal-take-off Reusable Launch Vehicle at Mach Numbers 1.60, 2.16, and 2.86 PDF full book. Access full book title Static Aerodynamic Characteristics of a Model of a Horizontal-take-off Reusable Launch Vehicle at Mach Numbers 1.60, 2.16, and 2.86 by . Download full books in PDF and EPUB format.

Static Aerodynamic Characteristics of a Model of a Horizontal-take-off Reusable Launch Vehicle at Mach Numbers 1.60, 2.16, and 2.86

Static Aerodynamic Characteristics of a Model of a Horizontal-take-off Reusable Launch Vehicle at Mach Numbers 1.60, 2.16, and 2.86 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 52

Get Book Here

Book Description

Static Aerodynamic Characteristics of a Model of a Horizontal-take-off Reusable Launch Vehicle at Mach Numbers 1.60, 2.16, and 2.86

Static Aerodynamic Characteristics of a Model of a Horizontal-take-off Reusable Launch Vehicle at Mach Numbers 1.60, 2.16, and 2.86 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 52

Get Book Here

Book Description

Longitudinal Aerodynamic Characteristics of a Model of a Horizontal Take Off Reusable Launch Vehicle at Mach Numbers from 3 to 6

Longitudinal Aerodynamic Characteristics of a Model of a Horizontal Take Off Reusable Launch Vehicle at Mach Numbers from 3 to 6 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 46

Get Book Here

Book Description

Lateral Aerodynamic Characteristics of a Conceptual Horizontal-take-off Reusable Launch Vehicle from Mach 3 to 6

Lateral Aerodynamic Characteristics of a Conceptual Horizontal-take-off Reusable Launch Vehicle from Mach 3 to 6 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 44

Get Book Here

Book Description

Wind-tunnel Investigation at Mach Numbers from 0.60 to 1.20 of the Static Aerodynamic Characteristics of a Model of a Possible Nonlifting Reentry Capsule in Combination with a Rocket Booster

Wind-tunnel Investigation at Mach Numbers from 0.60 to 1.20 of the Static Aerodynamic Characteristics of a Model of a Possible Nonlifting Reentry Capsule in Combination with a Rocket Booster PDF Author: Albin O. Pearson
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 22

Get Book Here

Book Description

Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing

Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing PDF Author: Edward J. Ray
Publisher:
ISBN:
Category :
Languages : en
Pages : 88

Get Book Here

Book Description

Investigation of the Static Longitudinal Aerodynamic Characteristics of a 1/10-scale Model of the Blue Scout Jr. at Mach Numbers from 0.40 to 1.03

Investigation of the Static Longitudinal Aerodynamic Characteristics of a 1/10-scale Model of the Blue Scout Jr. at Mach Numbers from 0.40 to 1.03 PDF Author: Thomas C. Kelly
Publisher:
ISBN:
Category : Launch vehicles (Astronautics)
Languages : en
Pages : 80

Get Book Here

Book Description

Aerodynamic Characteristics of a Complete VTO Launch Vehicle and Reusable Flyback Configuration from Mach 3.0 to 6.0

Aerodynamic Characteristics of a Complete VTO Launch Vehicle and Reusable Flyback Configuration from Mach 3.0 to 6.0 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 52

Get Book Here

Book Description

Static Aerodynamic Characteristics of a Series of Generalized Slender Bodies with and Without Fins at Mach Numbers Form 0.6 to 3.0 and Angles of Attack from 0 to 180 Deg

Static Aerodynamic Characteristics of a Series of Generalized Slender Bodies with and Without Fins at Mach Numbers Form 0.6 to 3.0 and Angles of Attack from 0 to 180 Deg PDF Author: William B. Baker (Jr.)
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 450

Get Book Here

Book Description

Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0.065-scale Model of a Four-stage Rocket Configuration at Mach Numbers of 1.41 and 1.82

Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0.065-scale Model of a Four-stage Rocket Configuration at Mach Numbers of 1.41 and 1.82 PDF Author: Ross B. Robinson
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 42

Get Book Here

Book Description

Aerodynamic Loading Characteristics at Mach Numbers from 0.80 to 1.20 of a 1/10-scale Three-stage Scout Model

Aerodynamic Loading Characteristics at Mach Numbers from 0.80 to 1.20 of a 1/10-scale Three-stage Scout Model PDF Author: Thomas C. Kelly
Publisher:
ISBN:
Category : Launch vehicles (Astronautics)
Languages : en
Pages : 68

Get Book Here

Book Description
Aerodynamic loads results have been obtained in the Langley 8-foot transonic pressure tunnel at Mach numbers from 0.80 to 1.20 for a 1/10-scale model of the upper three stages of the Scout vehicle. Tests were conducted through an angle-of-attack range from -8° to 8° at an average test Reynolds number per foot of about 4.0 x 106. Results indicated that the peak negative pressures associated with expansion corners at the nose and transition flare exhibit sizeable variations which occur over a relatively small Mach number range. The magnitude of the variations may cause the critical local loading condition for the full-scale vehicle to occur at a Mach number considerably lower than that at which the maximum dynamic pressure occurs in flight. The addition of protuberances simulating antennas and wiring conduits had slight, localized effects. The lift carryover from the nose and transition flare on the cylindrical portions of the model generally increased with an increase in Mach number.