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Book Supersonic Longitudinal Aerodynamic Characteristics of Two Space Shuttle Orbiter Configurations   conducted in the Langley Unitary Plan Wind Tunnel

Download or read book Supersonic Longitudinal Aerodynamic Characteristics of Two Space Shuttle Orbiter Configurations conducted in the Langley Unitary Plan Wind Tunnel written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-09 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted to determine the supersonic longitudinal aerodynamic characteristics of 0.015 scale models of the Rockwell International 089B and 139B space shuttle orbiter configurations and the 139B orbiter with a modifier forebody. The models each had a 45 deg swept delta wing that was blended into the body with an 81 deg swept fillet to form a double delta planform. The vertical tail had a split rudder deflected 27.5 deg on each side to form a speed brake. Tests were conducted at Mach numbers of 2.5, 3.9, and 4.6 at a Reynolds number, based on the body length of the 089B model, of 4,150,000. Angles of attack varied from -4 deg to 44 deg at 0 deg sideslip. Ellison, J. C. Langley Research Center NASA-TM-74074, L-11787 RTOP 506-26-30-04...

Book Supersonic and Hypersonic Aerodynamic Characteristics of Two Shuttle Orbiter Configurations Designed for Reduced Length

Download or read book Supersonic and Hypersonic Aerodynamic Characteristics of Two Shuttle Orbiter Configurations Designed for Reduced Length written by and published by . This book was released on 1974 with total page 55 pages. Available in PDF, EPUB and Kindle. Book excerpt: Performance, stability, and control tests at supersonic and hypersonic speeds have been performed on two versions of a shuttle orbiter configuration designed for reduced length. One of the test configurations had twin dorsal fins rolled out 15 deg, the other a centerline single dorsal fin. Effects of eleven and body flap deflection, rudder flare, planform fillet, and aileron deflection were examined. The supersonic tests were over the Mach number range from 1.6 to 4.63 at a Reynolds number based on model length of 4.3 x 10(exp 6). The hypersonic tests were conducted at a Mach number of 10.3 and Reynolds number of 0.67 x 10(exp 6). Aerodynamics, Supersonic and hypersonic, Space vehicles.

Book Supersonic Longitudinal Stability Characteristics of the Two Final Stages of a Four stage Launch Vehicle

Download or read book Supersonic Longitudinal Stability Characteristics of the Two Final Stages of a Four stage Launch Vehicle written by Royce L. McKinney and published by . This book was released on 1964 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Supersonic Aerodynamic Characteristics of a Two staged Space Shuttle Model Having a Delta wing Orbiter Mated Atop a Winged Booster

Download or read book Supersonic Aerodynamic Characteristics of a Two staged Space Shuttle Model Having a Delta wing Orbiter Mated Atop a Winged Booster written by Ernald B. Graves and published by . This book was released on 1972 with total page 259 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book SUPERSONIC AERODYNAMIC CHARACTERISTICS OF A TWO STAGED SPACE SHUTTLE MODEL HAVING A DELTA WING ORBITER MATED ATOP A WINGED BOOSTER

Download or read book SUPERSONIC AERODYNAMIC CHARACTERISTICS OF A TWO STAGED SPACE SHUTTLE MODEL HAVING A DELTA WING ORBITER MATED ATOP A WINGED BOOSTER written by UNITED STATES. NATIONAL AERONAUTICS AND SPACE ADMINISTRATION. and published by . This book was released on 1966 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book The Static and Dynamic Longitudinal Stability Characteristics of Some Supersonic Aircraft Configurations

Download or read book The Static and Dynamic Longitudinal Stability Characteristics of Some Supersonic Aircraft Configurations written by Jesse L. Mitchell and published by . This book was released on 1952 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Technical Memorandum

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1977 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Supersonic Longitudinal Aerodynamic Characteristics of Two Wing body Configurations Employing Warped Arrow Wings of Varying Dihedral

Download or read book Supersonic Longitudinal Aerodynamic Characteristics of Two Wing body Configurations Employing Warped Arrow Wings of Varying Dihedral written by Wilber D. Middleton and published by . This book was released on 1963 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 702 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Characteristics of a Tailless Fixed wing Supersonic Transport Configuration at Mach Number 2 20

Download or read book Aerodynamic Characteristics of a Tailless Fixed wing Supersonic Transport Configuration at Mach Number 2 20 written by Gerald V. Foster and published by . This book was released on 1964 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Interference Effects of Aft Reaction control Yaw Jets on the Aerodynamic Characteristics of a Space Shuttle Orbiter Model at Supersonic Speeds

Download or read book Interference Effects of Aft Reaction control Yaw Jets on the Aerodynamic Characteristics of a Space Shuttle Orbiter Model at Supersonic Speeds written by Peter F. Covell and published by . This book was released on 1983 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt: