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 /

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

Effects of wing planform on the aerodynamic characteristics of a wing-body-tail model at Mach numbers 1.57, 2.16, and 2.87 /

McKinney, Royce L.
Jernell, Lloyd S.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1965

"March 1965."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effect at M = 1.60 of nacelle shape and position on the aerodynamic characteristics in pitch of two wing-body combinations with a 47©� sweptback wings /

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

January 1952

"Januayr 12, 1952."Includes bibliographical references (p. 7).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

Aerodynamic loading characteristics in sideslip of a 45©� sweptback wing with and without a fence at high subsonic speeds /

Kuhn, Richard E.
Byrnes, Andrew L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"January 28, 1955."Includes bibliographical references (p. 9).Mode of access: Internet

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

Dunning, Robert W.
Smith, Fred M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1959

"June 11, 1953; Declassified August 26, 1959."Includes bibliographical references (p. 6).Mode of acc...

Transonic wind-tunnel investigation of the effects of aspect ratio, spanwise variations in section thickness ratio, and a body indentation on the aerodynamic characteristics of a 45©� sweptback wing-body combination /

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

January 1953

" January 27, 1953."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 wing incidence on the longitudinal trim characteristics of a cambered 70° delta-wing configuration at mach numbers 3.0 to 5.0 /

Ahtye, Warren F.
Ames Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

Wind-tunnel investigation of the effects of steady rolling on the aerodynamic loading characteristics of a 45©� sweptback wing at high subsonic speeds /

Wiggins, James W.
Kuhn, Richard E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1954

"November 6, 1953."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

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

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...

Effect of wing-mounted external stores on the lift and drag of the Douglas D-558-II research airplane at transonic speeds /

Nugent, Jack.
Flight Research Center (U.S.)
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1957

"July 17, 1957."Includes bibliographical references (p. 10).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

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

Effects of wing planform on the aerodynamic characteristics of a wing-body-tail model at Mach numbers 1.57, 2.16, and 2.87 /

McKinney, Royce L.
Jernell, Lloyd S.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1965

"March 1965."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effect at M = 1.60 of nacelle shape and position on the aerodynamic characteristics in pitch of two wing-body combinations with a 47©� sweptback wings /

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

January 1952

"Januayr 12, 1952."Includes bibliographical references (p. 7).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

Aerodynamic loading characteristics in sideslip of a 45©� sweptback wing with and without a fence at high subsonic speeds /

Kuhn, Richard E.
Byrnes, Andrew L.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"January 28, 1955."Includes bibliographical references (p. 9).Mode of access: Internet

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

Dunning, Robert W.
Smith, Fred M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1959

"June 11, 1953; Declassified August 26, 1959."Includes bibliographical references (p. 6).Mode of acc...

Transonic wind-tunnel investigation of the effects of aspect ratio, spanwise variations in section thickness ratio, and a body indentation on the aerodynamic characteristics of a 45©� sweptback wing-body combination /

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

January 1953

" January 27, 1953."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 wing incidence on the longitudinal trim characteristics of a cambered 70° delta-wing configuration at mach numbers 3.0 to 5.0 /

Ahtye, Warren F.
Ames Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

Wind-tunnel investigation of the effects of steady rolling on the aerodynamic loading characteristics of a 45©� sweptback wing at high subsonic speeds /

Wiggins, James W.
Kuhn, Richard E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1954

"November 6, 1953."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

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

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...

Effect of wing-mounted external stores on the lift and drag of the Douglas D-558-II research airplane at transonic speeds /

Nugent, Jack.
Flight Research Center (U.S.)
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1957

"July 17, 1957."Includes bibliographical references (p. 10).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

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

Effects of wing planform on the aerodynamic characteristics of a wing-body-tail model at Mach numbers 1.57, 2.16, and 2.87 /

McKinney, Royce L.
Jernell, Lloyd S.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1965

"March 1965."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effect at M = 1.60 of nacelle shape and position on the aerodynamic characteristics in pitch of two wing-body combinations with a 47©� sweptback wings /

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

January 1952

"Januayr 12, 1952."Includes bibliographical references (p. 7).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 /

Abstract

Extracted data

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 /

Abstract

Extracted data

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