Author: Frank S. Malvestuto (Jr.)Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 282
Book Description
Study to Determine Aerodynamic Characteristics on Hypersonic Re-entry Configurations
Author: Frank S. Malvestuto (Jr.)Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 282
Book Description
Tests to Determine Subsonic Aerodynamic Characteristics of Hypersonic Re-entry Configurations
Author: K. MantzPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 252
Book Description
WADC Technical Report
Author: United States. Wright Air Development DivisionPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1246
Book Description
Hypersonic Aerodynamic Characteristics of a Reentry Configuration with Variable-sweep Wings
Author: Measurement of Aerodynamic Characteristics of Re-entry Configuratioons in Free Flight at Hypersonic and Near-orbital Speeds
Author: R. L. NELSONPublisher:
ISBN:
Category :
Languages : en
Pages : 27
Book Description
URATIONS IN RE-ENTRY FLIGHT AT VERY HIGH SPEEDS HAS REQUIRED EXTENSIONS OF TECHNIQUES DEVELOPED EARLIER FOR AIRCRAFT AND LOW-SPEED MISSILES. EXTENSIONS ARE MADE FROM RECENT THEORETICAL STUDIES OF RE-ENTRY MECHANICS AND DYNAMICS AND THEIR APPLICATION TO FLIGHT MEASUREMENTS. EMPHASIS IS PLACED ON THE REDUCTION OF FLIGHT OSCILLATION DATA TO OBTAIN STATIC PITCHING MOMENT AND DAMPING DATA. HIGHLY NONLINEAR CHARACTERISTICS ARE ASSUMED. THROUGH APPLICATION OF THE PROCEDURE TO FLIGHT DATA AND A DIGITAL-COMPUTER SOLUTION, THE REDUCTION TECHNIQUE IS SHOWN TO BE ADEQUATE FOR RE-ENTRY CONFIGURATIONS TRIMMED ABOUT ZERO ANGLE-OF-ATTACK.
Hypersonic Aerodynamic Performances of Asymmetric Re-Entry Vehicles
Author: Mukkarum HusainPublisher: LAP Lambert Academic Publishing
ISBN: 9783845406374
Category :
Languages : en
Pages : 100
Book Description
Maneuverability of re-entry vehicles can be improved notably simply by modifying the geometric characteristics of the vehicles. The objective of the present work is to study the aerodynamic characteristics of different asymmetric re-entry vehicles. An algorithm based on Yee, Sandham, and Djomehri's high resolution, low dissipation numerical scheme is constructed, and the associated computational code is developed. This developed code is then validated by different test cases. Aerodynamic performances of asymmetric re-entry vehicles with different configurations and orientations are computed using the low dissipative high resolution artificial compression method. Upper portion of a symmetrical blunt body is cut by three different plane surfaces at three different locations to generate asymmetric blunt bodies. Effects of cutting plane angles and locations are studied. Present study shows that, for a given range of angles of attack and flight conditions, improved lift and stability in longitudinal plane and better control in transverse plane can be achieved by generating appropriate asymmetric re-entry vehicles.
NASA Technical Memorandum
Author: Supersonic Aerodynamic Characteristics of Some Reentry Concepts for Angles of Attack to 90 Deg
Author: Transonic, Supersonic and Hypersonic Wind-tunnel Tests on Aerodynamic Characteristics of Reentry Body with Blunted Cone Configuration
Author: Kojiro SuzukiPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 25
Book Description
Author: