Read Transonic Aerodynamic Characteristics of a Proposed Wing-Body Reusable Launch Vehicle Concept

Transonic Aerodynamic Characteristics of a Proposed Wing-Body Reusable Launch Vehicle Concept

National Aeronautics and Space Administration

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Description:A proposed wing-body reusable launch vehicle was tested in the NASA Marshall Space Flight Center's 14 x 14-inch trisonic wind tunnel during the winter of 1994. This test resulted in the vehicle's subsonic and transonic, Mach 0.3 to 1.96, longitudinal and lateral aerodynamic characteristics. The effects of control surface deflections on the basic vehicle's aerodynamics, including a body flap, elevons, ailerons, and tip fins, are presented. Springer, A. M. Marshall Space Flight Center AERODYNAMIC CHARACTERISTICS; AERODYNAMIC FORCES; AERODYNAMIC STABILITY; ANGLE OF ATTACK; BODY-WING CONFIGURATIONS; CONTROL SURFACES; LATERAL STABILITY; LONGITUDINAL STABILITY; MACH NUMBER; SIDESLIP; SINGLE STAGE TO ORBIT VEHICLES; SPACECRAFT STABILITY; SUBSONIC SPEED; TRANSONIC SPEED; WIND TUNNEL TESTS; AILERONS; ELEVONS; FINS; PITCHING MOMENTS; ROLLING MOMENTS; YAWING MOMENTS...We have made it easy for you to find a PDF Ebooks without any digging. And by having access to our ebooks online or by storing it on your computer, you have convenient answers with Transonic Aerodynamic Characteristics of a Proposed Wing-Body Reusable Launch Vehicle Concept. To get started finding Transonic Aerodynamic Characteristics of a Proposed Wing-Body Reusable Launch Vehicle Concept, you are right to find our website which has a comprehensive collection of manuals listed.
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Pages: 118

Format: PDF, EPUB & Kindle Edition

Publisher: Createspace Independent Publishing Platform

Release: 2018

ISBN: 1723465372

Description: A proposed wing-body reusable launch vehicle was tested in the NASA Marshall Space Flight Center's 14 x 14-inch trisonic wind tunnel during the winter of 1994. This test resulted in the vehicle's subsonic and transonic, Mach 0.3 to 1.96, longitudinal and lateral aerodynamic characteristics. The effects of control surface deflections on the basic vehicle's aerodynamics, including a body flap, elevons, ailerons, and tip fins, are presented. Springer, A. M. Marshall Space Flight Center AERODYNAMIC CHARACTERISTICS; AERODYNAMIC FORCES; AERODYNAMIC STABILITY; ANGLE OF ATTACK; BODY-WING CONFIGURATIONS; CONTROL SURFACES; LATERAL STABILITY; LONGITUDINAL STABILITY; MACH NUMBER; SIDESLIP; SINGLE STAGE TO ORBIT VEHICLES; SPACECRAFT STABILITY; SUBSONIC SPEED; TRANSONIC SPEED; WIND TUNNEL TESTS; AILERONS; ELEVONS; FINS; PITCHING MOMENTS; ROLLING MOMENTS; YAWING MOMENTS...We have made it easy for you to find a PDF Ebooks without any digging. And by having access to our ebooks online or by storing it on your computer, you have convenient answers with Transonic Aerodynamic Characteristics of a Proposed Wing-Body Reusable Launch Vehicle Concept. To get started finding Transonic Aerodynamic Characteristics of a Proposed Wing-Body Reusable Launch Vehicle Concept, you are right to find our website which has a comprehensive collection of manuals listed.
Our library is the biggest of these that have literally hundreds of thousands of different products represented.

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Transonic Aerodynamic Characteristics of a Proposed Wing-Body Reusable Launch Vehicle Concept

Transonic Aerodynamic Characteristics of a Proposed Wing-Body Reusable Launch Vehicle Concept

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