Aerodynamic characteristics of two delta wings and two trapezoidal wings at Mach number of 4.04 /

The effects of fuselage size on the low-speed longitudinal aerodynamic characteristics of a thin 60©� delta wing with and without a double slotted flap /

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

January 1953

"February 2, 1953."Includes bibliographical references (p. 9-10).Mode of access: Internet

Characteristics at mach number of 2.03 of a series of wings having various spanwise distributions of thickness ration and chord /

Robins, A. Warner.
Jackson, Charlie M.
Harris, Roy V.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aircraft.Includes bibliographical references.Mode of access: Internet

The effects of wing incidence on the aerodynamic loading characteristics of a sweptback wing-body combination at transonic speeds /

Robinson, Harold L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"October 12, 1954; Declassified December 1, 1959."Includes bibliographical references (p. 11).Mode o...

The aerodynamic characteristics of several thick delta wings at Mach numbers to 6 and angles of attack 50° /

McDevitt, John B.
Rakich, John V.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"March 1960."Cover title.Includes bibliographical references (p. 26).Mode of access: Internet

Aerodynamic characteristics of several cranked leading-edge wing-body combinations at Mach numbers from 0.4 to 2.94 /

Hopkins, Edward J.
Carmichael, Ralph L.
Hicks, Raymond M.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1967

"October 1967."Includes bibliographical references (p.21).Mode of access: Internet

A note on the drag due to lift of delta wings at Mach numbers up to 2.0 /

Osborne, Robert S.
Kelly, Thomas C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"April 9, 1953."Includes bibliographical references (p. 7-9).Mode of access: Internet

Aerodynamic characteristics over a Mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2©� delta wing and an unswept horizontal tail. /

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

January 1958

"March 6, 1958."Includes bibliographical references (p. 13).Mode of access: Internet

Aerodynamic characteristics at small scale and a Mach number of 1.38 of untapered wings having M and W plan forms /

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

January 1954

"June 18, 1954."Includes bibliographical references (p. 8).Mode of access: Internet

Aerodynamic characteristics at mach numbers of 1.41 and 2.01 of a series of cranked wings ranging in aspect ratio from 4.00 to 1.74 in combination with a body /

Sevier, John R.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Effects of size of external stores on the aerodynamic characteristics of an unswept and a 45©� sweptback wing of aspect ratio 4 and a 60©� delta wing at Mach numbers of 1.41, 1.62, and 1.96 /

Jacobsen, Carl R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"January 21, 1953."Includes bibliographical references (p. 8-9).Mode of access: Internet

A tabulation of wind-tunnel pressure data and section aerodynamic characteristics at Mach numbers of 1.61 and 2.01 for two trapezoidal and three delta wings having different surface shapes /

Landrum, Emma Jean.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft;Stresses and loads.Includes bibliograp...

Aerodynamic characteristics at Mach numbers from 1.6 to 2.8 of 74⁰ swept arrow wings with and without camber and twist /

Hasson, Dennis F.
Wong, Norman.
Fichter, Ann B.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical reference (p. 9).Mode of access: Internet

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.01 of a tailless delta V/STOL configuration having variable-sweep wing panels /

Spearman, M. Leroy.
Foster, Gerald V.
Langley Research Center.

January 1961

"December 1961."Cover title.Includes bibliographical references (p. 8).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

Pressure distributions on blunt-delta wings at angles of attack up to 90 degrees and Mach number of 6.85 /

Bernot, Peter T.
United States. National Aeronautics and Space Administration.

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

The effects of fuselage size on the low-speed longitudinal aerodynamic characteristics of a thin 60©� delta wing with and without a double slotted flap /

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

January 1953

"February 2, 1953."Includes bibliographical references (p. 9-10).Mode of access: Internet

Characteristics at mach number of 2.03 of a series of wings having various spanwise distributions of thickness ration and chord /

Robins, A. Warner.
Jackson, Charlie M.
Harris, Roy V.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aircraft.Includes bibliographical references.Mode of access: Internet

The effects of wing incidence on the aerodynamic loading characteristics of a sweptback wing-body combination at transonic speeds /

Robinson, Harold L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"October 12, 1954; Declassified December 1, 1959."Includes bibliographical references (p. 11).Mode o...

The aerodynamic characteristics of several thick delta wings at Mach numbers to 6 and angles of attack 50° /

McDevitt, John B.
Rakich, John V.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"March 1960."Cover title.Includes bibliographical references (p. 26).Mode of access: Internet

Aerodynamic characteristics of several cranked leading-edge wing-body combinations at Mach numbers from 0.4 to 2.94 /

Hopkins, Edward J.
Carmichael, Ralph L.
Hicks, Raymond M.
United States. National Aeronautics and Space Administration.
Ames Research Center.

January 1967

"October 1967."Includes bibliographical references (p.21).Mode of access: Internet

A note on the drag due to lift of delta wings at Mach numbers up to 2.0 /

Osborne, Robert S.
Kelly, Thomas C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"April 9, 1953."Includes bibliographical references (p. 7-9).Mode of access: Internet

Aerodynamic characteristics over a Mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2©� delta wing and an unswept horizontal tail. /

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

January 1958

"March 6, 1958."Includes bibliographical references (p. 13).Mode of access: Internet

Aerodynamic characteristics at small scale and a Mach number of 1.38 of untapered wings having M and W plan forms /

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

January 1954

"June 18, 1954."Includes bibliographical references (p. 8).Mode of access: Internet

Aerodynamic characteristics at mach numbers of 1.41 and 2.01 of a series of cranked wings ranging in aspect ratio from 4.00 to 1.74 in combination with a body /

Sevier, John R.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Effects of size of external stores on the aerodynamic characteristics of an unswept and a 45©� sweptback wing of aspect ratio 4 and a 60©� delta wing at Mach numbers of 1.41, 1.62, and 1.96 /

Jacobsen, Carl R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"January 21, 1953."Includes bibliographical references (p. 8-9).Mode of access: Internet

A tabulation of wind-tunnel pressure data and section aerodynamic characteristics at Mach numbers of 1.61 and 2.01 for two trapezoidal and three delta wings having different surface shapes /

Landrum, Emma Jean.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft;Stresses and loads.Includes bibliograp...

Aerodynamic characteristics at Mach numbers from 1.6 to 2.8 of 74⁰ swept arrow wings with and without camber and twist /

Hasson, Dennis F.
Wong, Norman.
Fichter, Ann B.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical reference (p. 9).Mode of access: Internet

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.01 of a tailless delta V/STOL configuration having variable-sweep wing panels /

Spearman, M. Leroy.
Foster, Gerald V.
Langley Research Center.

January 1961

"December 1961."Cover title.Includes bibliographical references (p. 8).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

Pressure distributions on blunt-delta wings at angles of attack up to 90 degrees and Mach number of 6.85 /

Bernot, Peter T.
United States. National Aeronautics and Space Administration.

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

The effects of fuselage size on the low-speed longitudinal aerodynamic characteristics of a thin 60©� delta wing with and without a double slotted flap /

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

January 1953

"February 2, 1953."Includes bibliographical references (p. 9-10).Mode of access: Internet

Characteristics at mach number of 2.03 of a series of wings having various spanwise distributions of thickness ration and chord /

Robins, A. Warner.
Jackson, Charlie M.
Harris, Roy V.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aircraft.Includes bibliographical references.Mode of access: Internet

The effects of wing incidence on the aerodynamic loading characteristics of a sweptback wing-body combination at transonic speeds /

Robinson, Harold L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"October 12, 1954; Declassified December 1, 1959."Includes bibliographical references (p. 11).Mode o...

Aerodynamic characteristics of two delta wings and two trapezoidal wings at Mach number of 4.04 /

Abstract

Extracted data

Aerodynamic characteristics of two delta wings and two trapezoidal wings at Mach number of 4.04 /

Abstract

Extracted data

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