Preliminary results of supersonic-jet tests of simplified wing structures /

Approximate solutions for the flow about flat-top wing-body configurations at high supersonic airspeeds /

Savin, Raymond C.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "September 15, 1958."Includes bibliographical references: p. 35-36.Mode of access: I...

An analysis of ducted-airfoil ram jets for supersonic aircraft /

Hill, Paul R.
Gammal, A. A.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1948

"July 7, 1948."Includes bibliographical references (p. 29).Mode of access: Internet

Transonic flight tests to determine the effect of thickness ratio and plan-form modification on the zero-lift drag of a 45©� sweptback wing /

Pepper, William B.
Hoffman, Sherwood.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"August 12, 1952."Includes bibliographical references (p. 9).Mode of access: Internet

Free-jet tests of a 1.1-inch-diameter supersonic ram-jet engine /

Judd, Joseph H.
Trout, Otto F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"March 5, 1952."Includes bibliographical references (p. 8).Mode of access: Internet

Investigation of wing flutter at transonic speeds for six systematically varied wing plan forms /

Jones, George W.
DuBose, Hugh C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"August 13, 1953."Includes bibliographical references (p. 15).Mode of access: Internet

Results of two experiments on flutter of high-aspect-ratio swept wings in the transonic speed range /

Lauten, William T.
O'Kelly, Burke R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"July 3, 1952."Includes bibliographical references (p. 8).Mode of access: Internet

Rocket-powered flight test of a roll-stabilized supersonic missile configuration /

Gardiner, Robert A.
Zarovsky, Jacob.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"January 12, 1950."Includes bibliographical references (p. 12).Mode of access: Internet

Langley 9-inch supersonic tunnel tests of several modifications of a supersonic missile having tandem cruciform lifting surfaces : three-component data results of models having ratios of wing span to tail span less than 1 /

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

January 1960

"March 7, 1951; Declassified July 28, 1960."Includes bibliographical references (p. 7).Mode of acces...

An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and a 40©� sweepback : pressure distribution measurements of the interference effect of the wing on the fuselage at Mach numbers of 1.40 and 1.59 /

Gapcynski, John P.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
Clark, James W.

January 1952

"July 17, 1952."Includes bibliographical references (p. 8).Mode of access: Internet

Preliminary results of the flight investigation between Mach numbers of 0.80 and 1.36 of a rocket-powered model of a supersonic airplane configuration having a tapered wing with circular-arc sections and 40©� sweepback /

D'Aiutolo, Charles T.
Mason, Homer P.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"October 31, 1950. Declassified September 17, 1958."Cover title.Includes bibliographical references ...

Transonic wind-tunnel investigation of an unswept wing in combination with a systematic series of four bodies /

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

January 1953

"Janauary 6, 1953."Includes bibliographical references (p. 11).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

Large-scale flight measurements of zero-lift drag and low-lift drag of 10 wing-body configurations at Mach numbers from 0.8 to 1.6 /

Morrow, John D.
Nelson, Robert L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"January 15, 1953."Includes bibliographical references (p. 12-13).Mode of access: Internet

Investigation of pitch maneuver speed margins for a supersonic transport configuration with a variable-sweep wing /

Sawyer, Richard H.
Silsby, Norman S.
McLaughlin, Milton D.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

"October 1967."Includes bibliographical references (p. 15).Mode of access: Internet

The effects of a small jet of air exhausting from the nose of a body of revolution in supersonic flow /

Love, Eugene S.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"November 12, 1952."Includes bibliographical references (p. 16).Mode of access: Internet

Approximate solutions for the flow about flat-top wing-body configurations at high supersonic airspeeds /

Savin, Raymond C.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "September 15, 1958."Includes bibliographical references: p. 35-36.Mode of access: I...

An analysis of ducted-airfoil ram jets for supersonic aircraft /

Hill, Paul R.
Gammal, A. A.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1948

"July 7, 1948."Includes bibliographical references (p. 29).Mode of access: Internet

Transonic flight tests to determine the effect of thickness ratio and plan-form modification on the zero-lift drag of a 45©� sweptback wing /

Pepper, William B.
Hoffman, Sherwood.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"August 12, 1952."Includes bibliographical references (p. 9).Mode of access: Internet

Free-jet tests of a 1.1-inch-diameter supersonic ram-jet engine /

Judd, Joseph H.
Trout, Otto F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"March 5, 1952."Includes bibliographical references (p. 8).Mode of access: Internet

Investigation of wing flutter at transonic speeds for six systematically varied wing plan forms /

Jones, George W.
DuBose, Hugh C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"August 13, 1953."Includes bibliographical references (p. 15).Mode of access: Internet

Results of two experiments on flutter of high-aspect-ratio swept wings in the transonic speed range /

Lauten, William T.
O'Kelly, Burke R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"July 3, 1952."Includes bibliographical references (p. 8).Mode of access: Internet

Rocket-powered flight test of a roll-stabilized supersonic missile configuration /

Gardiner, Robert A.
Zarovsky, Jacob.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"January 12, 1950."Includes bibliographical references (p. 12).Mode of access: Internet

Langley 9-inch supersonic tunnel tests of several modifications of a supersonic missile having tandem cruciform lifting surfaces : three-component data results of models having ratios of wing span to tail span less than 1 /

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

January 1960

"March 7, 1951; Declassified July 28, 1960."Includes bibliographical references (p. 7).Mode of acces...

An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and a 40©� sweepback : pressure distribution measurements of the interference effect of the wing on the fuselage at Mach numbers of 1.40 and 1.59 /

Gapcynski, John P.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
Clark, James W.

January 1952

"July 17, 1952."Includes bibliographical references (p. 8).Mode of access: Internet

Preliminary results of the flight investigation between Mach numbers of 0.80 and 1.36 of a rocket-powered model of a supersonic airplane configuration having a tapered wing with circular-arc sections and 40©� sweepback /

D'Aiutolo, Charles T.
Mason, Homer P.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"October 31, 1950. Declassified September 17, 1958."Cover title.Includes bibliographical references ...

Transonic wind-tunnel investigation of an unswept wing in combination with a systematic series of four bodies /

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

January 1953

"Janauary 6, 1953."Includes bibliographical references (p. 11).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

Large-scale flight measurements of zero-lift drag and low-lift drag of 10 wing-body configurations at Mach numbers from 0.8 to 1.6 /

Morrow, John D.
Nelson, Robert L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"January 15, 1953."Includes bibliographical references (p. 12-13).Mode of access: Internet

Investigation of pitch maneuver speed margins for a supersonic transport configuration with a variable-sweep wing /

Sawyer, Richard H.
Silsby, Norman S.
McLaughlin, Milton D.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

"October 1967."Includes bibliographical references (p. 15).Mode of access: Internet

The effects of a small jet of air exhausting from the nose of a body of revolution in supersonic flow /

Love, Eugene S.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"November 12, 1952."Includes bibliographical references (p. 16).Mode of access: Internet

Approximate solutions for the flow about flat-top wing-body configurations at high supersonic airspeeds /

Savin, Raymond C.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "September 15, 1958."Includes bibliographical references: p. 35-36.Mode of access: I...

An analysis of ducted-airfoil ram jets for supersonic aircraft /

Hill, Paul R.
Gammal, A. A.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1948

"July 7, 1948."Includes bibliographical references (p. 29).Mode of access: Internet

Transonic flight tests to determine the effect of thickness ratio and plan-form modification on the zero-lift drag of a 45©� sweptback wing /

Pepper, William B.
Hoffman, Sherwood.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"August 12, 1952."Includes bibliographical references (p. 9).Mode of access: Internet

Preliminary results of supersonic-jet tests of simplified wing structures /

Abstract

Extracted data

Preliminary results of supersonic-jet tests of simplified wing structures /

Abstract

Extracted data

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