Longitudinal and Lateral Stability and Control Characteristics at Mach Number 2.01 of a 60 Degree Delta-Wing Airplane Configuration Equipped With a Canard Control and With Wing Trailing-Edge Flap Controls

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

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Description

Memorandum presenting an investigation in the 4- by 4-foot supersonic pressure tunnel at Mach number 2.01 to determine the longitudinal and lateral stability and control characteristics of a 60 degree delta-wing airplane configuration equipped with a trapezoidal canard control and with wing trailing-edge flap controls. The investigation included studies of the flap control with and without canard surface and studies of the canard control alone and with the flap control.

Physical Description

51 p. : ill.

Creation Information

Spearman, M. Leroy & Driver, Cornelius March 10, 1958.

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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 245 times . More information about this report can be viewed below.

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  • Main Title: Longitudinal and Lateral Stability and Control Characteristics at Mach Number 2.01 of a 60 Degree Delta-Wing Airplane Configuration Equipped With a Canard Control and With Wing Trailing-Edge Flap Controls
  • Series Title: NACA Research Memorandums

Description

Memorandum presenting an investigation in the 4- by 4-foot supersonic pressure tunnel at Mach number 2.01 to determine the longitudinal and lateral stability and control characteristics of a 60 degree delta-wing airplane configuration equipped with a trapezoidal canard control and with wing trailing-edge flap controls. The investigation included studies of the flap control with and without canard surface and studies of the canard control alone and with the flap control.

Physical Description

51 p. : ill.

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  • Accession or Local Control No: 93R19175
  • URL: http://hdl.handle.net/2060/19930089885 External Link
  • Report No.: NACA-RM-L58A20
  • Center for AeroSpace Information Number: 19930089885
  • Archival Resource Key: ark:/67531/metadc63755

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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

  • March 10, 1958

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

Description Last Updated

  • Aug. 21, 2018, 3:44 p.m.

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Spearman, M. Leroy & Driver, Cornelius. Longitudinal and Lateral Stability and Control Characteristics at Mach Number 2.01 of a 60 Degree Delta-Wing Airplane Configuration Equipped With a Canard Control and With Wing Trailing-Edge Flap Controls, report, March 10, 1958; (digital.library.unt.edu/ark:/67531/metadc63755/: accessed October 19, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.