Effects of various modifications on the static longitudinal stability and control characteristics of a 0.065-scale model of the Chance Vought Regulus II missile at a Mach number of 2.01: TED No. NACA AD 398

One of 5,164 reports in the series: NACA Research Memorandums available on this site.

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Description

Report presenting an investigation in the 4- by 4-foot supersonic pressure tunnel to determine the effects on the static longitudinal stability and control characteristics of various modifications to a 0.065-scale model of the Chance Vought Regulus II missile. Some of the modifications included control housing on top of the fuselage, two sizes of canard surfaces with fixed incidence angles, various angles of nose droop, and two types of inlet boundary-layer bleed diverters.

Physical Description

[26] p. : ill.

Creation Information

Robinson, Ross B. & Driver, Cornelius September 26, 1955.

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This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and one other and was provided by UNT Libraries Government Documents Department to Digital Library, a digital repository hosted by the UNT Libraries. It has been viewed 38 times . More information about this report can be viewed below.

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  • Main Title: Effects of various modifications on the static longitudinal stability and control characteristics of a 0.065-scale model of the Chance Vought Regulus II missile at a Mach number of 2.01: TED No. NACA AD 398
  • Series Title: NACA Research Memorandums

Description

Report presenting an investigation in the 4- by 4-foot supersonic pressure tunnel to determine the effects on the static longitudinal stability and control characteristics of various modifications to a 0.065-scale model of the Chance Vought Regulus II missile. Some of the modifications included control housing on top of the fuselage, two sizes of canard surfaces with fixed incidence angles, various angles of nose droop, and two types of inlet boundary-layer bleed diverters.

Physical Description

[26] p. : ill.

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  • Accession or Local Control No: 93R18172
  • URL: http://hdl.handle.net/2060/19930088882 External Link
  • Report No.: NACA-RM-SL55I15
  • Center for AeroSpace Information Number: 19930088882
  • Archival Resource Key: ark:/67531/metadc61628

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National Advisory Committee for Aeronautics Collection

The National Advisory Committee for Aeronautics (NACA) was a U.S. federal agency founded on March 3, 1915 to undertake, promote, and institutionalize aeronautical research. On October 1, 1958 the agency was dissolved, and its assets and personnel transferred to the newly created National Aeronautics and Space Administration (NASA).

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Creation Date

  • September 26, 1955

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

Description Last Updated

  • July 16, 2018, 4:30 p.m.

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Robinson, Ross B. & Driver, Cornelius. Effects of various modifications on the static longitudinal stability and control characteristics of a 0.065-scale model of the Chance Vought Regulus II missile at a Mach number of 2.01: TED No. NACA AD 398, report, September 26, 1955; (digital.library.unt.edu/ark:/67531/metadc61628/: accessed October 19, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.