Development of NACA submerged inlets and a comparison with wing leading-edge inlets for a 1/4-scale model of a fighter airplane /

United States naval aviation, 1910-1980 /

Armstrong, William J.
Van Vleet, Clarke.
United States. Naval Air Systems Command.
United States. Office of the Chief of Naval Operations

January 1981

Includes indexes."Supersedes NAVWEPS 00-80P-1 dated 1970.""NAVAIR 00-80P-1."Authors: Clarke Van Vlee...

Air-flow surveys in the vicinity of representative NACA 1-series cowlings /

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

January 1948

"May 7, 1948."Includes bibliographical references (p. 12).Mode of access: Internet

The performance of conical supersonic scoop inlets on circular fuselages /

Hasel, Lowell E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"November 17, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

An experimental investigation of NACA submerged air inlets on a 1/5-scale model of a fighter airplane /

Gault, Donald E.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "December 5, 1947."Includes bibliographical references: p. 9.Mode of access: Interne...

Tests of submerged duct installation on a modified fighter airplane in the Ames 40- by 80-foot wind tunnel /

Martin, Norman J.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "December 11, 1947."Includes bibliographical references: p. 7.Mode of access: Intern...

Some factors affecting the variation of pitching moment with sideslip of aircraft configurations /

Polhamus, Edward C.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NACA Research Abstract No. 115. ...

NAVFAC index to engineering & design criteria.

United States. Naval Facilities Engineering Command.

January 1984

Cover title.Includes indexes."December 1983.""This revision of NAVFAC DM-50 cancels and supersedes a...

Free-flight measurements of the rolling effectiveness and drag of trailing-edge spoilers on a tapered sweptback wing at Mach numbers between 0.6 and 1.4 /

Schult, Eugene D.
Fields, E. M.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NACA Research Abstract No. 111. ...

Jet effects on longitudinal trim of an airplane configuration measured at Mach numbers between 1.2 and 1.8 /

Peck, Robert F.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NACA Research Abstract No. 121. ...

NAVFAC index to engineering & design criteria.

United States. Naval Facilities Engineering Command.
United States. Naval Facilities Engineering Command.

January 1982

"This revision of NAVFAC DM-50 cancels and supersedes all prior issues"--P. iv."September 1981."Cove...

Development of flow distortions in a full-scale nacelle inlet at mach numbers 0.63 and 1.6 to 2.0 /

Piercy, Thomas G.
Chiccine, Bruce G.
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, 1955."Includes bibliographical references (p. 16-17).Mode of access: Internet

Investigation over moving ground plane of a transport airplane model using blowing over flaps for boundary-layer control /

Vogler, Raymond D.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).Mode of access: Internet

Investigation of water-pond arresting of a dynamic model of a jet transport /

Thompson, William C.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft; Aircraft safety and noise; Piloting;Includes bibliographical refere...

NAVFAC index to engineering & design criteria.

United States. Naval Facilities Engineering Command.

"This revision of NAVFAC DM-50 cancels and supersedes all prior issues"--P. 50-iii.Includes indexes....

Wind-tunnel investigation at high subsonic speeds of the effect of spoiler profile on the lateral control characteristics of a wing-fuselage combination winter quarter-chord line swept back 32.6©� and NACA 65A006 airfoil section /

Johnson, Harold S.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NASA Technical Publications Anno...

United States naval aviation, 1910-1980 /

Armstrong, William J.
Van Vleet, Clarke.
United States. Naval Air Systems Command.
United States. Office of the Chief of Naval Operations

January 1981

Includes indexes."Supersedes NAVWEPS 00-80P-1 dated 1970.""NAVAIR 00-80P-1."Authors: Clarke Van Vlee...

Air-flow surveys in the vicinity of representative NACA 1-series cowlings /

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

January 1948

"May 7, 1948."Includes bibliographical references (p. 12).Mode of access: Internet

The performance of conical supersonic scoop inlets on circular fuselages /

Hasel, Lowell E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"November 17, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

An experimental investigation of NACA submerged air inlets on a 1/5-scale model of a fighter airplane /

Gault, Donald E.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "December 5, 1947."Includes bibliographical references: p. 9.Mode of access: Interne...

Tests of submerged duct installation on a modified fighter airplane in the Ames 40- by 80-foot wind tunnel /

Martin, Norman J.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "December 11, 1947."Includes bibliographical references: p. 7.Mode of access: Intern...

Some factors affecting the variation of pitching moment with sideslip of aircraft configurations /

Polhamus, Edward C.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NACA Research Abstract No. 115. ...

NAVFAC index to engineering & design criteria.

United States. Naval Facilities Engineering Command.

January 1984

Cover title.Includes indexes."December 1983.""This revision of NAVFAC DM-50 cancels and supersedes a...

Free-flight measurements of the rolling effectiveness and drag of trailing-edge spoilers on a tapered sweptback wing at Mach numbers between 0.6 and 1.4 /

Schult, Eugene D.
Fields, E. M.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NACA Research Abstract No. 111. ...

Jet effects on longitudinal trim of an airplane configuration measured at Mach numbers between 1.2 and 1.8 /

Peck, Robert F.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NACA Research Abstract No. 121. ...

NAVFAC index to engineering & design criteria.

United States. Naval Facilities Engineering Command.
United States. Naval Facilities Engineering Command.

January 1982

"This revision of NAVFAC DM-50 cancels and supersedes all prior issues"--P. iv."September 1981."Cove...

Development of flow distortions in a full-scale nacelle inlet at mach numbers 0.63 and 1.6 to 2.0 /

Piercy, Thomas G.
Chiccine, Bruce G.
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, 1955."Includes bibliographical references (p. 16-17).Mode of access: Internet

Investigation over moving ground plane of a transport airplane model using blowing over flaps for boundary-layer control /

Vogler, Raymond D.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."August 1967."Includes bibliographical references (p. 10).Mode of access: Internet

Investigation of water-pond arresting of a dynamic model of a jet transport /

Thompson, William C.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft; Aircraft safety and noise; Piloting;Includes bibliographical refere...

NAVFAC index to engineering & design criteria.

United States. Naval Facilities Engineering Command.

"This revision of NAVFAC DM-50 cancels and supersedes all prior issues"--P. 50-iii.Includes indexes....

Wind-tunnel investigation at high subsonic speeds of the effect of spoiler profile on the lateral control characteristics of a wing-fuselage combination winter quarter-chord line swept back 32.6©� and NACA 65A006 airfoil section /

Johnson, Harold S.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

On front cover: "Classification Changed to Unclassified, Authority: NASA Technical Publications Anno...

United States naval aviation, 1910-1980 /

Armstrong, William J.
Van Vleet, Clarke.
United States. Naval Air Systems Command.
United States. Office of the Chief of Naval Operations

January 1981

Includes indexes."Supersedes NAVWEPS 00-80P-1 dated 1970.""NAVAIR 00-80P-1."Authors: Clarke Van Vlee...

Air-flow surveys in the vicinity of representative NACA 1-series cowlings /

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

January 1948

"May 7, 1948."Includes bibliographical references (p. 12).Mode of access: Internet

The performance of conical supersonic scoop inlets on circular fuselages /

Hasel, Lowell E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"November 17, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

Development of NACA submerged inlets and a comparison with wing leading-edge inlets for a 1/4-scale model of a fighter airplane /

Abstract

Extracted data

Development of NACA submerged inlets and a comparison with wing leading-edge inlets for a 1/4-scale model of a fighter airplane /

Abstract

Extracted data

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