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Book
Experimental stagnation-point velocity gradients and heat-transfer coefficients for a family of blunt bodies at Mach 8 and angles of attack
Authors: --- ---
Year: 1969 Publisher: Washington, D.C. : National Aeronautics and Space Administration,

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Descriptions and operating parameters of a Mach 2 nozzle system for the Langley 11-inch ceramic-heated tunnel
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Year: 1968 Publisher: Washington, D.C. : National Aeronautics and Space Administration,

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Aerodynamic characteristics of the NACA 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10⁶ to 8.0 x 10⁶
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Year: 1954 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,

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Exploratory investigation of flow field resulting from forward-facing nozzles exhausting near a large cylindrical body at free-stream Mach numbers of 3.0 and 6.0
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Year: 1969 Publisher: Washington, D.C. : National Aeronautics and Space Administration,

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The aerodynamic design and calibration of an asymmetric variable Mach number nozzle with a sliding block for the Mach number range 1.27 to 2.75
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Year: 1953 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,

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Effect of shape changes on the aerodynamic characteristics of a twisted and cambered arrow wing at Mach number 2.03
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Year: 1968 Publisher: Washington, D.C. : National Aeronautics and Space Administration,

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Simulation of two projectiles connected by a flexible tether
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Year: 2000 Publisher: Aberdeen Proving Ground, MD : Army Research Laboratory,

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Book
Effect of speed brakes on the supersonic aerodynamic characteristics of a variable-sweep tactical fighter model at Mach numbers from 1.60 to 2.50
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Year: 1968 Publisher: Washington, D.C. : National Aeronautics and Space Administration,

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Book
Airfoil section characteristics at high angles of attack
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Year: 1954 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,

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Book
Hypersonic vehicles : past, present and future developments
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ISBN: 1839622709 1839622695 Year: 2019 Publisher: London, United Kingdom : IntechOpen,

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