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An experimental pressure-distribution investigation of interference effects produced at a Mach number of 3.11 by wedge- shaped bodies located under a triangular wing / by Lowell E. Has [Leather Bound]

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An experimental pressure-distribution investigation of interference effects produced at a Mach number of 3.11 by wedge- shaped bodies located under a triangular wing / by Lowell E. Has [Leather Bound]

Lowell E. Hasel

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An experimental pressure-distribution investigation of interference effects produced at a Mach number of 3.11 by wedge- shaped bodies located under a triangular wing / by Lowell E. Has [Leather Bound]

An experimental pressure-distribution investigation of interference effects produced at a Mach number of 3.11 by wedge- shaped bodies located under a triangular wing / by Lowell E. Has [Leather Bound]

More Books

The performance of conical supersonic scoop inlets on circular fuselages / By Lowell E. Hasel. 1953 [Leather Bound]

The performance of conical supersonic scoop inlets on circular fuselages / By Lowell E. Hasel. 1953 [Leather Bound]

Analysis of the performance of the drive system and diffuser of the Langley Unitary Plan Wind Tunnel / Lowell E. Hasel and Robert L. Stallings, Jr. 1981 [Leather Bound]

Analysis of the performance of the drive system and diffuser of the Langley Unitary Plan Wind Tunnel / Lowell E. Hasel and Robert L. Stallings, Jr. 1981 [Leather Bound]

Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effect at M = 1.60 o [Leather Bound]

Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effect at M = 1.60 o [Leather Bound]