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Box 1

 Container

Contains 17 Collections and/or Records:

Lana Murphy Couch papers

 Collection — Multiple Containers
Identifier: MSA 312
Scope and Contents The Lana Murphy Couch papers document Couch's forty year career with NASA, first as a wind tunnel test engineer, and later in management positions. Types of materials include: correspondence, newsletters, papers, photographs, programs, publications, research and work reports, technical reports, VHS tapes, writings, and material related to award recognition.
Dates: 1953 - 1997; Majority of material found within 1970 - 1995

Writings and Publications, 1966 - 1980

 Series — Box: 1
Identifier: MSA 312, Series 1
Scope and Contents Contained within this series are NASA technical reports, memoranda, and notes, along with conference papers, articles, and working papers that Couch authored or co-authored.
Dates: 1966 - 1980

Couch, L. C.; Stallings, R. L. Jr.; Collins, I. K. Heat-Transfer Measurements on a Flat Plate With Attached Protuberances in a Turbulent Boundary Layer at MACH Numbers of 2.49, 3.51, and 4.44. NASA TN D-3736. Washington, DC: National Aeronautics and Space Administration, December 1966

 Item — Box: 1, Item: 1
Identifier: MSA 312, Series 1, Item 1
Scope and Contents From the Series: Contained within this series are NASA technical reports, memoranda, and notes, along with conference papers, articles, and working papers that Couch authored or co-authored.
Dates: December 1966

Morris, W. D.; Couch, L. M. Experimental Pressure Distributions on a Blunt Lifting-Entry Body at MACH 3.71. NASA TN D-4494. Washington, DC: National Aeronautics and Space Administration, April 1968

 Item — Box: 1, Item: 2
Identifier: MSA 312, Series 1, Item 2
Scope and Contents From the Series: Contained within this series are NASA technical reports, memoranda, and notes, along with conference papers, articles, and working papers that Couch authored or co-authored.
Dates: April 1968

Couch, L. M. Flow-Field Measurements Downstream of Two Protuberances on a Flat Plate Submerged in a Turbulent Boundary Layer at MACH 2.49 and 4.44. NASA TN D-5287. Washington, DC: National Aeronautics and Space Administration, July 1969

 Item — Box: 1, Item: 3
Identifier: MSA 312, Series 1, Item 3
Scope and Contents From the Series: Contained within this series are NASA technical reports, memoranda, and notes, along with conference papers, articles, and working papers that Couch authored or co-authored.
Dates: July 1969

Couch, L. M. Transonic Wall Interference Effects on Bodies of Revolution; AIAA 7th Aerodynamic Testing Conference, Palo Alto, California, September 13-15, 1972. New York, New York: American Institute of Aeronautics and Astronautics, 1972

 Item — Box: 1, Item: 4
Identifier: MSA 312, Series 1, Item 4
Scope and Contents From the Series: Contained within this series are NASA technical reports, memoranda, and notes, along with conference papers, articles, and working papers that Couch authored or co-authored.
Dates: 1972

Couch, L. M.; Brooks, C. W. Jr. Effect of Blockage Ratio on Drag and Pressure Distributions for Bodies of Revolution at Transonic Speeds. NASA TN D-7331. Washington, DC: National Aeronautics and Space Administration, November 1973

 Item — Box: 1, Item: 5
Identifier: MSA 312, Series 1, Item 5
Scope and Contents From the Series: Contained within this series are NASA technical reports, memoranda, and notes, along with conference papers, articles, and working papers that Couch authored or co-authored.
Dates: November 1973

Couch, L. M. Drag and Stability Characteristics of a Variety of Reefed and Unreefed Parachute Configurations at MACH 1.80 with an Empirical Correlation for Supersonic MACH Numbers. NASA TR R-429. Washington, DC: National Aeronautics and Space Administration, February 1975

 Item — Box: 1, Item: 6
Identifier: MSA 312, Series 1, Item 6
Scope and Contents From the Series: Contained within this series are NASA technical reports, memoranda, and notes, along with conference papers, articles, and working papers that Couch authored or co-authored.
Dates: February 1975

Nugent, J.; Couch, L. M.; Webb, L. D. Exploratory Wind Tunnel Tests of a Shock-Swallowing Air Data Sensor at a MACH Number of Approximately 1.83. TM X-56030. Edwards, California: NASA Flight Research Center, March 1975

 Item — Box: 1, Item: 7
Identifier: MSA 312, Series 1, Item 7
Scope and Contents From the Series: Contained within this series are NASA technical reports, memoranda, and notes, along with conference papers, articles, and working papers that Couch authored or co-authored.
Dates: March 1975

Couch, L. M. Geometric Optimization of the Supersonic Stagnation-Pressure Probe; Presented at the Instrument Society of America 21st International Instrumentation Symposium, Philadelphia, PA, May 19 - 21, 1975.

 Item — Box: 1, Item: 9
Identifier: MSA 312, Series 1, Item 9
Scope and Contents From the Series: Contained within this series are NASA technical reports, memoranda, and notes, along with conference papers, articles, and working papers that Couch authored or co-authored.
Dates: May 19 - 21, 1975.

Meyers, J. F.; Couch, L. M.; Feller, W. V. Laser Velcocimeter Measurements in a Large Transonic Wind Tunnel; Presented at the Symposium on Laser Anemometry, Bloomington, MN, October 22 - 24, 1975

 Item — Box: 1, Item: 10
Identifier: MSA 312, Series 1, Item 10
Scope and Contents From the Series: Contained within this series are NASA technical reports, memoranda, and notes, along with conference papers, articles, and working papers that Couch authored or co-authored.
Dates: 1975

Couch, L. M. Geometric Optimization of the Supersonic Stagnation-Pressure Probe. Reprinted from ISA Transactions, Volume 15, Number 1, 1976

 Item — Box: 1, Item: 11
Identifier: MSA 312, Series 1, Item 11
Scope and Contents From the Series: Contained within this series are NASA technical reports, memoranda, and notes, along with conference papers, articles, and working papers that Couch authored or co-authored.
Dates: 1976

Couch, L. M.; Wieting, A. R. Capability for Aerothermal-Structural Tests of Large-To-Full-Scale Components of Future Space Transportation Systems. Presented at the AIAA Conference on Advanced Technology for Future Space Systems, May 8-11, 1979, Langley Research Center, Hampton, Virginia, 1976

 Item — Box: 1, Item: 12
Identifier: MSA 312, Series 1, Item 12
Scope and Contents From the Series: Contained within this series are NASA technical reports, memoranda, and notes, along with conference papers, articles, and working papers that Couch authored or co-authored.
Dates: 1976

Camarda, C. J.; Couch, L. M.; Kelly, H. N. Heat Pipes Cool Probe and Sandwich Panel. NASA Tech Briefs, Winter 1980

 Item — Box: 1, Item: 13
Identifier: MSA 312, Series 1, Item 13
Scope and Contents From the Series: Contained within this series are NASA technical reports, memoranda, and notes, along with conference papers, articles, and working papers that Couch authored or co-authored.
Dates: Winter 1980

Couch, L. M. A New Approach to Providing Additional MACH Number Capacity for the 8-FT. HTST, Thermal Structures Branch, undated

 Item — Box: 1, Item: 14
Identifier: MSA 312, Series 1, Item 14
Scope and Contents From the Series: Contained within this series are NASA technical reports, memoranda, and notes, along with conference papers, articles, and working papers that Couch authored or co-authored.
Dates: undated

Stallings, R. L. Jr.; Couch, L. M.; Tudor, D. H. Langley Working Paper, Experimental Pressure Distributions on a 120º Cone at MACH Numbers from 2.96 to 4.63 and Angles of Attack from 0º to 20º, undated

 Item — Box: 1, Item: 15
Identifier: MSA 312, Series 1, Item 15
Scope and Contents From the Series: Contained within this series are NASA technical reports, memoranda, and notes, along with conference papers, articles, and working papers that Couch authored or co-authored.
Dates: undated