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981.
|
The composition of the basaltic gas phase [NASA TR R-348]
by Nordlie, Bert E. Material type:  Book Description: 81p.Publisher: Washington, D.C. National aeronautics and space administration 1971Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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982.
|
Diffusion reacting air counette flow with hydrogen injection [NASA TR R-349]
by Graves, Randolphb A. Material type: Book Description: 51p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1970Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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983.
|
Declination radial distance and phases of the moon for the years 1961 to 1971 for use in trajectory considerations [NASA TN D-911]
by Woolston, Donald S. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 48p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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984.
|
Wind tunnel investigation of a ballons as Towed decelaration at mach numbers from 1.47 to 2.50 [NASA TN D-919]
by Mcshera, John T | Keyes, J.Wayne. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 75p.Publisher: Washigton, D. C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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985.
|
Stability and control characterstics of a small scale model of an aerial vehicle supported by two ducted fans [NASA TN D-920]
by Parlett, Lysle P. Material type: Book Description: 22p.Publisher: Washingtom National aeronautics and space administration Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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986.
|
Cyclic furnace oxidation of clad WI-52systems at 1040 degree and 1090 degree C [NASA TN D -6730]
by Gedwiil, , Michael A. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 29p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1972Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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987.
|
An efficent algorithm using matrix methods to solve wind tunnel force balance [NASA TN D-686-79]
by Smith,David L. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 43p.Publisher: Washington, D.C. National aeronautics and space administration 1972Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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988.
|
Light detection electronics for a raman lidar [NASA TN D-6879]
by Leser,Robert J | Salzman,Jack A. Material type: Book Description: 27p.Publisher: Washington,D.C. National aeronautics and space administration 1972Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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989.
|
Summary of design considerations for airplane spin recovery parachute systems [NASA TN D -6866]
by Burk,Sanger M | Jr. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 53p.Publisher: Washington ;D. C. National aeronautics and space administration Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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990.
|
Progreesof NASA resarch relatin to noise allleviaton of large subsonic jet aircrafft [NASA SP=189]
by Proceedings ... Conference held at large subsonc jet aircraft Hampton, Virgina 8-10, 1968. Material type: Book; Format:
print
; Literary form:
not fiction
Publisher: Washington, D C. National Aeronautics and Space Adminstration 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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991.
|
Dynamic stability and dispersion of a project mercury test capsule upon entering the atmosphere , with effects of roll rate centre of gravity diplacement, and threshold of a rate reaction control system [NASA TM X-350]
by Jaquet, Byron M. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 78p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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992.
|
An experimental study of the flutter of sails having a a delta planform tested from a macnh number of 0.1 to A mach number of 1.9 [NASA TM X-355]
by Hess, Robert W. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 39p.Publisher: Washington, D. C National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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993.
|
Wind tunnel investigationof the static and dynamicrotary stability derivativesofa fllat top wing body model at mach numbers of 2.5, 3.0 and 3.5 [NASA TM X-361]
by Lampkin, Bedford A | Endicott, Kenneth C. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 41p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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994.
|
The effects of wing plan from on the the static longitudinal aerodynamic characteristics of a flat-top hypersonicaircraft at mach numbers from 0.6 to 1.4 [NASA TM X-364]
by Treon, Stuart L. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 31p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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995.
|
Investigation at mach numbers of 0.20 to 3.50 of blended wing combinations of sonic design with diamond, delta and arrow plan from [NASA TM X-372]
by Holdway, George H | Mellenthin, Jack A. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 77p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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|
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996.
|
Investigation at mach numbers of 0.20 to 3.50 of blended wing body combinations of sonic design with diamond delta and arrow plan forms [NASA TM X
by Holdaway, George H | Mellenthin, Jack A. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 77p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: No items available
|
|
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997.
|
Free flight measurements of static and dynamic stability of models of the project mercury re-entry capsule at mach numbers 3 and 9.5 [NASA TM X-373]
by Sommer, Simon C | Short, Barbara J | Compton, Dale L. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 41p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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998.
|
Evaluation of blended wing body combinations with curved plan forms at mach numbersn uoto 3.50 [NASA TM X-379]
by Holdaway, George H | Mellenthin, Jack A. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 69p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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999.
|
Experimental perfromance of area ratio 200,25 and 8 nozzles on JP-4 fuel and liquid oxygen rocket engine [NASA TM X-382]
by Lovell, Calvin Lowell | Lovell, J. Calvin, Samanich, Nick A. and Barnett, Donald O | Calvin, Lovell, J | Donald O,,Barnett. Material type: Book Description: 75p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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1000.
|
Investigation at mach numbers of .60 to 3.50 of blended wing body combinationswith cambered and twisted wings with diamond, delta and arrow plan forms [NASA TM X-390]
by Holdaway, George H | Mellenthin, Jack A. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 76p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1961Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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