Mutual aerodynamic interference effects for multiple bodies by the cross-flow corrections method /

Some aerodynamic effects of blunting a projectile nose /

Dickinson, Elizabeth R.
U.S. Army Ballistic Research Laboratory.
U.S. Atomic Energy Commission.

"RDT & E Project No. 1M523801A287.""September 1964."Includes bibliographical references (page 22).Mo...

Interference effects at transonic speeds of jets exhausting from the hull step of a model of a large, water-based airplane /

Henry, Beverly Z.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 10).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...

Mutual aerodynamic interference effects for two axisymmetric bodies /

Martin, Fred W., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.

"The work described in this report was done during the period from September 1972 through June 1973 ...

Mutual aerodynamic interference effects for multiple bodies of revolution and distorted bodies of revolution /

Martin, Fred W., author.
Cutchins, Malcolm A., author.
Saunders, Grady. Jr., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.
Auburn University. Department of Aerospace Engineering. sponsor.

"April 1976."Includes bibliographical references (page 47).Print reproduction.Air Force Contract No....

Aerodynamic interference effects caused by parallel-staged simple aerodynamic configurations at Mach numbers of 3 and 6 /

Decker, John P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Aerodynamic characteristics effected by parallel- staged simple aerodynamic configurations at Mach n...

Interference effects of canard controls on the longitudinal aerodynamic characteristics of a winged body at Mach 10 /

Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 11).Mode of access: Internet

Induced interference effects on a four-jet VTOL configuration with various wing planforms in the transition speed range /

Otis, James H.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

Sting-support interference on longitudinal aerodynamic characteristics of cargo-type airplane models at Mach 0.70 to 0.84 /

Loving, Donald L.
Luoma, Arvo A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 13).Mode of access: Internet

Axial-force reduction by interference between jet and neighboring afterbody /

Pitts, William C.
Wiggins, Lyle E.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, missiles and space vehicles.Includes bibliographical refe...

Induced interference effects on the aerodynamic characteristics of a 0.16-scale six-jet V / by Matthew M. Winston.

Winston, Matthew M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1970

Work performed at Langley Research Center.N70-22633.Cover title.Includes bibliographical references ...

Theoretical investigation of the aerodynamic interference induced by cruise and lift fans on transport-type aircraft /

Mendenhall, M. R.
Spangler, Selden B.
Dillenius, Marnix F. E., 1938-
United States. National Aeronautics and Space Administration.
Ames Research Center.
Nielsen Engineering & Research.

January 1971

"Prepared by Nielsen Engineering & Research, Inc. ... for Ames Research Center."Cover title.Includes...

Influence of the body flow field on the zero-lift wave drag of wing-body combinations modified in accordance with the transonic area rule /

Page, William A.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "February 7, 1956."Includes bibliographical references: p. 19-20.Mode of access: Int...

Interference between exhaust system and afterbody of twin-engine fuselage configurations /

Runckel, Jack F.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16-17).Mode ...

Jet array impingement with crossflow - correlation of streamwise resolved flow and heat transfer distributions /

Florschuetz, L. W.
Truman, C. R.
Metzger, Darryl E., 1937-
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"Prepared for Lewis Research Center under Grant NSG-3075."Jan. 1981.Includes bibliographical referen...

Some aerodynamic effects of blunting a projectile nose /

Dickinson, Elizabeth R.
U.S. Army Ballistic Research Laboratory.
U.S. Atomic Energy Commission.

"RDT & E Project No. 1M523801A287.""September 1964."Includes bibliographical references (page 22).Mo...

Interference effects at transonic speeds of jets exhausting from the hull step of a model of a large, water-based airplane /

Henry, Beverly Z.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 10).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...

Mutual aerodynamic interference effects for two axisymmetric bodies /

Martin, Fred W., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.

"The work described in this report was done during the period from September 1972 through June 1973 ...

Mutual aerodynamic interference effects for multiple bodies of revolution and distorted bodies of revolution /

Martin, Fred W., author.
Cutchins, Malcolm A., author.
Saunders, Grady. Jr., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.
Auburn University. Department of Aerospace Engineering. sponsor.

"April 1976."Includes bibliographical references (page 47).Print reproduction.Air Force Contract No....

Aerodynamic interference effects caused by parallel-staged simple aerodynamic configurations at Mach numbers of 3 and 6 /

Decker, John P.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1969

Aerodynamic characteristics effected by parallel- staged simple aerodynamic configurations at Mach n...

Interference effects of canard controls on the longitudinal aerodynamic characteristics of a winged body at Mach 10 /

Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 11).Mode of access: Internet

Induced interference effects on a four-jet VTOL configuration with various wing planforms in the transition speed range /

Otis, James H.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

Sting-support interference on longitudinal aerodynamic characteristics of cargo-type airplane models at Mach 0.70 to 0.84 /

Loving, Donald L.
Luoma, Arvo A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 13).Mode of access: Internet

Axial-force reduction by interference between jet and neighboring afterbody /

Pitts, William C.
Wiggins, Lyle E.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, missiles and space vehicles.Includes bibliographical refe...

Induced interference effects on the aerodynamic characteristics of a 0.16-scale six-jet V / by Matthew M. Winston.

Winston, Matthew M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1970

Work performed at Langley Research Center.N70-22633.Cover title.Includes bibliographical references ...

Theoretical investigation of the aerodynamic interference induced by cruise and lift fans on transport-type aircraft /

Mendenhall, M. R.
Spangler, Selden B.
Dillenius, Marnix F. E., 1938-
United States. National Aeronautics and Space Administration.
Ames Research Center.
Nielsen Engineering & Research.

January 1971

"Prepared by Nielsen Engineering & Research, Inc. ... for Ames Research Center."Cover title.Includes...

Influence of the body flow field on the zero-lift wave drag of wing-body combinations modified in accordance with the transonic area rule /

Page, William A.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "February 7, 1956."Includes bibliographical references: p. 19-20.Mode of access: Int...

Interference between exhaust system and afterbody of twin-engine fuselage configurations /

Runckel, Jack F.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16-17).Mode ...

Jet array impingement with crossflow - correlation of streamwise resolved flow and heat transfer distributions /

Florschuetz, L. W.
Truman, C. R.
Metzger, Darryl E., 1937-
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"Prepared for Lewis Research Center under Grant NSG-3075."Jan. 1981.Includes bibliographical referen...

Some aerodynamic effects of blunting a projectile nose /

Dickinson, Elizabeth R.
U.S. Army Ballistic Research Laboratory.
U.S. Atomic Energy Commission.

"RDT & E Project No. 1M523801A287.""September 1964."Includes bibliographical references (page 22).Mo...

Interference effects at transonic speeds of jets exhausting from the hull step of a model of a large, water-based airplane /

Henry, Beverly Z.
United States. National Aeronautics and Space Administration.

"January 1960."Cover title.Includes bibliographical references (p. 10).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...

Mutual aerodynamic interference effects for multiple bodies by the cross-flow corrections method /

Abstract

Extracted data

Mutual aerodynamic interference effects for multiple bodies by the cross-flow corrections method /

Abstract

Extracted data

Related items

Related items