The development of an 8-inch by 8-inch slotted tunnel for Mach numbers up to 1.28 /

Description of recent changes in the Langley 6- by 28-inch transonic tunnel /

Sewall, William G.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 09."May 1981"--Cover."Langley Research Center."Includes bibliographical references....

Tunneling by machinery : description of perforators and plans of operations in mining and tunneling /

Haupt, Herman, 1817-1905.
Exposition universelle de 1867 à Paris.

January 1867

Prepared in explanation of the machines for mining and tunneling, forwarded for exhibition at the Pa...

A hydraulic-powered platform for scaling high backs and walls /

Rose, Charles K.
Morris, Carl.
Utter, Stephen.
United States. Bureau of Mines.

"Int. - Bu. of Mines, Pgh., Pa. 6217"--p. 4."August 1954."Mode of access: Internet

The development of an 8-inch by 8-inch slotted tunnel from mach numbers up to 1.28 /

Little, B. H.
Cubbage, James M.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Fluid mechanics; Research and development facili...

Some considerations concerning inlets and ducted bodies at Mach numbers from 0.8 to 2.0 /

Sears, Richard I.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"November 24, 1953."Includes bibliographical references (p. 10-11).Mode of access: Internet

Comparison of lift-curve slopes for a model tested in two slotted tunnels of different sizes at high subsonic speeds /

Boswinkle, Robert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"June 23, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

Pressure measurements on a body of revolution in the Langley 16-foot transonic tunnel and a comparison with free-fall data /

Hallissy, Joseph M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"March 5, 1952."Includes bibliographical references (p. 9).Mode of access: Internet

Air-flow and power characteristics of the Langley 16-foot transonic tunnel with slotted test section /

Ward, Vernon G.
Pearson, Merwin D.
Whitcomb, Charles F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"July 21, 1952."Includes bibliographical references (p. 21).Mode of access: Internet

Design operation and testing capabilities of the Langley 11-inch ceramic-heated tunnel

Trout, Otto F.
United States. National Aeronautics and Space Administration.

Cover title."February 1963."Includes bibliographical references.Mode of access: Internet

An analysis of the pressure distribution measured on a body of revolution at transonic speeds in the slotted test section of the Langley 8-foot transonic tunnel /

Estabrooks, Bruce B.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"June 25, 1952."Includes bibliographical references (p. 23).Mode of access: Internet

Effect of diffusers, shrouds, and mass injection on the starting and operating characteristics of a Mach 5 free jet tunnel /

Molloy, John K.
Keyes, J. Wayne.
Mackley, Ernest A.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N 71-34243.Includes bibliographical references (p. 30).Mode of a...

Concept development of a Mach 4 high-speed civil transport /

Domack, Christopher S.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 7-8.Mode of access: Internet

Investigation of two-stage air-cooled turbine suitable for flight at mach number of 2.5.

Miser, James W.
Stewart, Warner L.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1956

"October 22, 1956."Includes bibliographical references (p. 17).Mode of access: Internet

Telemeter transmission at 219.5 megacycles from two rocket-powered models at Mach number up to 15.7 /

Graves, George B.
Markley, J. Thomas.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"July 28, 1958."Includes bibliographical references (p. 13).Mode of access: Internet

Description and calibration of the Langley 6- by 19-inch transonic tunnel /

Ladson, Charles L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 16-17.Mode of access: Internet

Description of recent changes in the Langley 6- by 28-inch transonic tunnel /

Sewall, William G.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 09."May 1981"--Cover."Langley Research Center."Includes bibliographical references....

Tunneling by machinery : description of perforators and plans of operations in mining and tunneling /

Haupt, Herman, 1817-1905.
Exposition universelle de 1867 à Paris.

January 1867

Prepared in explanation of the machines for mining and tunneling, forwarded for exhibition at the Pa...

A hydraulic-powered platform for scaling high backs and walls /

Rose, Charles K.
Morris, Carl.
Utter, Stephen.
United States. Bureau of Mines.

"Int. - Bu. of Mines, Pgh., Pa. 6217"--p. 4."August 1954."Mode of access: Internet

The development of an 8-inch by 8-inch slotted tunnel from mach numbers up to 1.28 /

Little, B. H.
Cubbage, James M.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Fluid mechanics; Research and development facili...

Some considerations concerning inlets and ducted bodies at Mach numbers from 0.8 to 2.0 /

Sears, Richard I.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"November 24, 1953."Includes bibliographical references (p. 10-11).Mode of access: Internet

Comparison of lift-curve slopes for a model tested in two slotted tunnels of different sizes at high subsonic speeds /

Boswinkle, Robert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"June 23, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

Pressure measurements on a body of revolution in the Langley 16-foot transonic tunnel and a comparison with free-fall data /

Hallissy, Joseph M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"March 5, 1952."Includes bibliographical references (p. 9).Mode of access: Internet

Air-flow and power characteristics of the Langley 16-foot transonic tunnel with slotted test section /

Ward, Vernon G.
Pearson, Merwin D.
Whitcomb, Charles F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"July 21, 1952."Includes bibliographical references (p. 21).Mode of access: Internet

Design operation and testing capabilities of the Langley 11-inch ceramic-heated tunnel

Trout, Otto F.
United States. National Aeronautics and Space Administration.

Cover title."February 1963."Includes bibliographical references.Mode of access: Internet

An analysis of the pressure distribution measured on a body of revolution at transonic speeds in the slotted test section of the Langley 8-foot transonic tunnel /

Estabrooks, Bruce B.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"June 25, 1952."Includes bibliographical references (p. 23).Mode of access: Internet

Effect of diffusers, shrouds, and mass injection on the starting and operating characteristics of a Mach 5 free jet tunnel /

Molloy, John K.
Keyes, J. Wayne.
Mackley, Ernest A.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1971

Prepared at Langley Research Center.N 71-34243.Includes bibliographical references (p. 30).Mode of a...

Concept development of a Mach 4 high-speed civil transport /

Domack, Christopher S.
Langley Research Center.

January 1990

Prepared at Langley Research Center.Bibliography: p. 7-8.Mode of access: Internet

Investigation of two-stage air-cooled turbine suitable for flight at mach number of 2.5.

Miser, James W.
Stewart, Warner L.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1956

"October 22, 1956."Includes bibliographical references (p. 17).Mode of access: Internet

Telemeter transmission at 219.5 megacycles from two rocket-powered models at Mach number up to 15.7 /

Graves, George B.
Markley, J. Thomas.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"July 28, 1958."Includes bibliographical references (p. 13).Mode of access: Internet

Description and calibration of the Langley 6- by 19-inch transonic tunnel /

Ladson, Charles L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 16-17.Mode of access: Internet

Description of recent changes in the Langley 6- by 28-inch transonic tunnel /

Sewall, William G.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Subject category 09."May 1981"--Cover."Langley Research Center."Includes bibliographical references....

Tunneling by machinery : description of perforators and plans of operations in mining and tunneling /

Haupt, Herman, 1817-1905.
Exposition universelle de 1867 à Paris.

January 1867

Prepared in explanation of the machines for mining and tunneling, forwarded for exhibition at the Pa...

A hydraulic-powered platform for scaling high backs and walls /

Rose, Charles K.
Morris, Carl.
Utter, Stephen.
United States. Bureau of Mines.

"Int. - Bu. of Mines, Pgh., Pa. 6217"--p. 4."August 1954."Mode of access: Internet

The development of an 8-inch by 8-inch slotted tunnel for Mach numbers up to 1.28 /

Abstract

Extracted data

The development of an 8-inch by 8-inch slotted tunnel for Mach numbers up to 1.28 /

Abstract

Extracted data

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