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Taunton River. Letter from the Secretary of War, transmitting communication from the Chief of Engineers, relative to the improvement of the Taunton River, Massachusetts, with a report thereon. March 27, 1868. -- Referred to the Committee on Commerce and ordered to be printed

United States | TIBKAT | 1868

Beteiligte: Smith, Jared A.

Railways at the Paris exposition

Smith, Willard A. | Engineering Index Backfile | 1899

The design and construction of high speed motor boats

Smith, James A. | Engineering Index Backfile | 1906

High-speed motor-boats

Smith, James A. | Engineering Index Backfile | 1906

DEFLOCCULATED GRAPHITE AS A MOTOR LUBRICANT

SMITH, MARCUS A. | SAE Technical Papers | 1914

MID-WEST SECTION PAPERS HEAVY-DUTY HIGH-SPEED ENGINE

SMITH, MARK A / GRINER, OTIS E | SAE Technical Papers | 1920

Anderson, R. C. / Smith, D. B. / Haddon, A. C. | Taylor & Francis Verlag | 1922

Tests on Built-Up Airplane Struts Having Initial Tension in Outside Fibers

Schwamb, T A / Smith, C S | NTRS | 1923

Point drag and total drag of navy struts no. 1 modified

Zahm, A F / Smith, R H / Hill, G C | NTRS | 1923

Tests on built-up airplane struts having initial tension in outside fibers

Schwamb, T. A. / Smith, C. S. | SLUB | 1923

Beteiligte: Schwamb, T. A. , Smith, C. S.

Application of electric propulsion to double-ended ferry-boats

Kennedy, A. / Smith, Frank V. | IEEE | 1925

Application of electric propulsion to double-ended ferry boats

Kennedy, Jr., A. / Smith, F.V. | Engineering Index Backfile | 1925

Air forces, moments, and damping on model of fleet airship Shenandoah

Zahm, A. F. / Smith, R. H. / Louden, F. A. | TIBKAT | 1925

Discussion at pacific coast convention: Application of electric propulsion to double-ended ferry-boats

Kennedy, A. / Smith, Glen H. | IEEE | 1926

Air Forces, Moments and Damping on Model of Fleet Airship Shenandoah

Zahm, A F / Smith, R H / Louden, F A | NTRS | 1926

MURRAY, M. A. / BERNELLE, FREDERIC / SMITH, A. W. et al. | Taylor & Francis Verlag | 1927

WOODS, E. A. / CLOWES, G. S. LAIRD / ANDERSON, R. C. et al. | Taylor & Francis Verlag | 1927

Savings pay for new terminal

Smith, A. | Engineering Index Backfile | 1929

Drag of C-Class Airship Hulls of Various Fineness Ratios

Zahm, A F / Smith, R H / Louden, F A | NTRS | 1929

JOHNS, A. W. / ROGERS, BERTRAM / BRUCE, R. STUART et al. | Taylor & Francis Verlag | 1929

SMITH, A. H. / LONGSDON, E. H. | Taylor & Francis Verlag | 1937

Diesel Lubricating Problems

Smith, A. E. / Stewart, J. P. | SAE Technical Papers | 1941

Elliott-Lysholm supercharger

Lysholm, A. / Smith, R.B. / Wilson, W.A. | Engineering Index Backfile | 1943

Elliott-Lysholm supercharger

Lysholm, A. / Smith, R.B. / Wilson, W.A. | Engineering Index Backfile | 1943

Elliott-Lysholm supercharger

Lysholm, A. / Smith, R.B. / Wilson, W.A. | Engineering Index Backfile | 1943

Elliott-Lysholm supercharger

Lysholm, A. / Smith, R.B. / Wilson, W.A. | Engineering Index Backfile | 1943

Elliott-Lysholm supercharger

Lysholm, A. / Smith, R.B. / Wilson, W.A. | Engineering Index Backfile | 1943

The ELLIOTT-LYSHOLM SUPERCHARGER

LYSHOLM, ALF / SMITH, RONALD B. / WILSON, W. A. | SAE Technical Papers | 1943

MORE LANDING FACILITIES - THE KEY TO PRIVATE AVIATION'S GROWTH

Wales, James A. / Smith, Lee H. | SAE Technical Papers | 1945

The Chemical Action of Oils on Single Crystals of Metals

Gwathmey, A T / Leidheiser, H / Smith, G P | NTRS | 1945

Grid sandwich panels in compression

Dale, F. A. / Smith, Roy C. T. | SLUB | 1945

Beteiligte: Dale, F. A. , Smith, Roy C. T.

Preliminary Examination of Hull Afterbody Ventilation

K. M. Tomaszewski / A. G. Smith / G. F. Chalmers | NTIS | 1946

Nuclear-Powered Flight. Chapter 1: Introduction and Summary

A. E. Ruark / A. C. Beer / E. A. Bonney et al. | NTIS | 1947

Stress distribution in a beam of orthotropic material subjected to a concentrated load

Smith, C B / Voss, A W | NTRS | 1948

Flight tests of apparatus for varying dihedral effect in flight

Kauffman, W.M. / Smith, A. / Liddell, Jr., C.J. et al. | Engineering Index Backfile | 1948

Aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10 6 to 11.0 x 10 6

Schaefer, Raymond F. / Smith, Hamilton A. | TIBKAT | 1949

Aerodynamic Characteristics of the NACA 8-H-12 Airfoil Section at Six Reynolds Numbers from 1.8 x 10(exp 6) to 11.0 x 10(exp 6).

Schaefer, Raymond F / Smith, Hamilton A | NTRS | 1949

Aerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 x 10 6 to 9.0 x 10 6

Loftin, Laurence K. / Smith, Hamilton A. | TIBKAT | 1949

Aerodynamic Characteristics of 15 NACA Airfoil Sections at Seven Reynolds Numbers from 0.7 x 10(exp 6) to 9.0 x 10(exp 6)

Loftin, Laurence K , Jr / Smith, Hamilton A | NTRS | 1949

Two-dimensional Aerodynamic Characteristics of 34 Miscellaneous Airfoil Sections

Loftin, Laurence K , Jr / Smith, Hamilton A | NTRS | 1949

Fuel Systems And Carburetors For Personal Aircraft

VOLZ, A. J. / BALIS, M. R. / SMITH, S. M. | SAE Technical Papers | 1949

Body Steel And Its Treatment

BURKHALTER, C. A. / ALTENBURGER, C. L. / SMITH, H. C. et al. | SAE Technical Papers | 1949

Aerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 + 10 6 to 9.0. x 10 6

Loftin, Laurence K. / Smith, Hamilton A. | SLUB | 1949

Beteiligte: Smith, Hamilton A.

Airport lighting

Smith, A. | Engineering Index Backfile | 1950

Model tests on a symmetrical wing

Smelt, R. / Smith, A. G. | TIBKAT | 1950

Aerodynamic characteristics at Reynolds numbers of 3.0 x 10 6 and 6.0 x 10 6 of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section

Smith, Hamilton A. / Schaefer, Raymond F. | TIBKAT | 1950

Aerodynamic Characteristics at Reynolds Numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of Three Airfoil Sections Formed by Cutting off Various Amounts from the Rear Portion of the NACA 0012 Airfoil Section

Smith, Hamilton A / Schaefer, Raymond F | NTRS | 1950

Apparatus for varying effective dihedral in flight with application to study of tolerable dihedral on conventional fighter airplane

Kauffman, W.M. / Liddell, Jr., C.J. / Smith, A. et al. | Engineering Index Backfile | 1950

Tabulated Pressure Coefficients and Aerodynamic Characteristics Measured on the Wing of the Bell X-1 Airplane in an Unaccelerated Stall and in Pull-ups at Mach Numbers of 0.74, 0.75, 0.94, and 0.97

Smith, Lawrence A | NTRS | 1951

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Section and 40 Degree Sweepback : a Pressure-distribution Study of the Aerodynamic Characteristics of the Wing at Mach Number 1.40

Smith, Norman F / Kainer, Julian H / Webster, Robert A | NTRS | 1951

Sparkes, F. N. / Smith, A. F. | TIBKAT | 1952

Investigations of the Behaviour of Aircraft When Making a Forced Landing on Water (Ditching)

A. G. Smith / C. H. Warren / D. F. Wright | NTIS | 1952

The hull launching tank (descriptive)

Smith, A. G. / Abel, G. C. / Morris, W. et al. | TIBKAT | 1952

A method for determining the water stability of a seaplane in take-off and landing

White, H. G. | TIBKAT | 1952

Beteiligte: Smith, A. G.

Thermal Shock Resistance and High-temperature Strength of a Molybdenum Disilicide - Aluminum Oxide Ceramic

Maxwell, W A / Smith, R W | NTRS | 1953